command: 
 C:\Program Files (x86)\Code_Saturne\4.0\libexec\code_saturne\cs_solver.exe --param first.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 4.0.6


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

  revision 4.0.6-m
  build 10/24/16 11:12:42
  MPI version 2.0 (MS-MPI)


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

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

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


Local case configuration:

  Date:                04/24/17 14:56:51
  Processor:           
  Directory:           C:\Users\GIFFARD_Q\Desktop\Stage GIFFARD Quentin\prise en main code_saturne\veriftherm\RESU\20170424-1456
  MPI ranks:           3 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    SCOTCH 6.0.0

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

 --- Physics
       NVAR   =              5 (Nb variables                )
       NSCAL  =              1 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              1 (Nb specific physics scalars )
       NPROCE =              6 (Nb cell properties          )


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


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

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

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.11786E+01 (Reference density           )
       VISCL0 =    0.18300E-04 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


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

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


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


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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =              0 (Turbulence model            )
       IDEUCH =              0 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

 --- Constants

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


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              2 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.10000E-02 (Minimum time step           )
       DTMAX  =    0.10000E+02 (Maximum time step           )
       DTREF  =    0.10000E-01 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Velocity              1  0.1000E+01
 Pressure              0  0.1000E+01
 TempC                 1  0.1000E+01
----------------------------

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

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

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


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

---------------------------------------------------------------------
 Variable          ICONV  IDIFF IDIFFT ISCHCV ISSTPC   BLENCV  THETAV
---------------------------------------------------------------------
 Velocity              1      1      1      1      0 0.10E+01 0.10E+01
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
 TempC                 1      1      1      1      0 0.10E+01 0.10E+01
-------------------------------------------------------------

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


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


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

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

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

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


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


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

       IMRGRA =              0 (Reconstruction mode         )
       ANOMAX =    0.78540E+00 (Non-ortho angle: limit for  )
                               (least squares ext. neighbors)

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Velocity            100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 TempC               100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Velocity              1     -1  0.1500E+01
 Pressure              1     -1  0.1500E+01
 TempC                 1     -1  0.1500E+01
-----------------------------------

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


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


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


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-07      1
 Pressure          0.1000E-07      1
 TempC             0.1000E-07      1
------------------------------------

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


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


 ** SCALARS
    -------

       ITBRRB =              0 (T or H reconstruction at bdy)

-------------------------------------------------------------
 Variable         Number ISCACP ITURT      VISLS0      SIGMAS
-------------------------------------------------------------
 TempC                 1      1      0  0.2495E-01  0.1000E+01
---------------------------------------------------------------------

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

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

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

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

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

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

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


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


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

 --- Restarted calculation
       ISUITE =              0 (1: restarted calculation    )
       ILEAUX =              1 (1: read  restart/auxiliary  )
       IECAUX =              1 (1: write checkpoint/auxiliary)


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =            100 (Final time step required    )

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


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


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

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

 --- Post-processed variables


Velocity
Pressure
TempC
CourantNb
FourierNb
total_pressure
Local Time Step
         --           --

 --- Probe history files
       NTHIST =             -1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =              0 (Number of probes     )
       NTHSAV =             -1 (Checkpoint frequency )

       Number Name                  Nb. probes (-1: all)
         2 Velocity[X]                   -1
         3 Velocity[Y]                   -1
         4 Velocity[Z]                   -1
         5 Pressure                      -1
         6 TempC                         -1
         8 LamVisc                       -1
         9 CourantNb                     -1
        10 FourierNb                     -1
        11 total_pressure                -1
        12 Local Time Step               -1
         --           --                --

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 TempC                          0
         9 CourantNb                   -999
        10 FourierNb                   -999
        11 total_pressure              -999
        12 Local Time Step             -999
         --           --                --

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


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


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

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


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


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

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


 Reading file:        mesh_input
 Finished reading:    mesh_input
 No "partition_input\domain_number_3" file available;

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

 Partitioning by space-filling curve: Morton (in bounding box).
  Number of cells per domain (histogramm):
    [     139852 ;     139853 ] =          3

 Partitioning finished (3.53 s)


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

 Halo construction with standard neighborhood
 ============================================

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

 Histogram of the number of cells per rank:

    minimum value =             139852
    maximum value =             139853

      1 : [     139852 ;     139853 ] =          3

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

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

    minimum value =             142692
    maximum value =             145441

      1 : [     142692 ;     143241 [ =          2
      2 : [     143241 ;     143791 [ =          0
      3 : [     143791 ;     144341 [ =          0
      4 : [     144341 ;     144891 [ =          0
      5 : [     144891 ;     145441 ] =          1

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

 Histogram of the number of ghost cells per rank:

    minimum value =               2839
    maximum value =               5589

      1 : [       2839 ;       3389 [ =          2
      2 : [       3389 ;       3939 [ =          0
      3 : [       3939 ;       4489 [ =          0
      4 : [       4489 ;       5039 [ =          0
      5 : [       5039 ;       5589 ] =          1

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

 Histogram of the number of interior faces per rank:

    minimum value =             271369
    maximum value =             273599

      1 : [     271369 ;     271815 [ =          2
      2 : [     271815 ;     272261 [ =          0
      3 : [     272261 ;     272707 [ =          0
      4 : [     272707 ;     273153 [ =          0
      5 : [     273153 ;     273599 ] =          1

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

 Histogram of the number of boundary faces per rank:

    minimum value =              19718
    maximum value =              20584

      1 : [      19718 ;      19891 [ =          1
      2 : [      19891 ;      20064 [ =          0
      3 : [      20064 ;      20237 [ =          0
      4 : [      20237 ;      20410 [ =          0
      5 : [      20410 ;      20584 ] =          2

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        999
      2 : [          3 ;          4 ] =     418558

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  2
    maximum value =                  2

      1 : [          2 ;          2 ] =          3

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

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

 Renumbering mesh:

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

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

   renumbering for boundary faces:
     numbering:                           none

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

 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =             140571
    maximum value =             143224

      1 : [     140571 ;     141101 [ =          1
      2 : [     141101 ;     141632 [ =          0
      3 : [     141632 ;     142162 [ =          1
      4 : [     142162 ;     142693 [ =          0
      5 : [     142693 ;     143224 ] =          1

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               1163
    maximum value =               1449

      1 : [       1163 ;       1220 [ =          1
      2 : [       1220 ;       1277 [ =          0
      3 : [       1277 ;       1334 [ =          0
      4 : [       1334 ;       1391 [ =          1
      5 : [       1391 ;       1449 ] =          1

 Mesh coordinates:               minimum    and maximum
                       X : 0.0000000e+000 1.0000000e+000
                       Y : 0.0000000e+000 4.0000000e-001
                       Z : 0.0000000e+000 1.0000000e-001
 Mesh
     Number of cells:          419557
     Number of interior faces: 808706
     Number of boundary faces: 60816
     Number of vertices:       85753

 Groups:
    "Inflow"
       boundary faces:         2296
    "Outflow"
       boundary faces:         2296
    "Symmetry"
       boundary faces:        22430
    "Wall"
       boundary faces:        33794

 --- Information on the volumes
       Minimum control volume      = 9.0100980e-009
       Maximum control volume      = 1.3545675e-006
       Total volume for the domain = 4.0000000e-002

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

  Criterion 2: Offset:
    Number of bad cells detected: 1802 -->   0 %

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 4 -->   0 %

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

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

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

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

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

 Computing geometric quantities (0.358 s)
                                                             
       ALMAX  =    0.34236E+00 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.


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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  TempC             0.3000E+03  0.3000E+03
 ---------------------------------

                dt  0.1000E-01  0.1000E-01
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E-01   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1179E+01  0.1179E+01
  molecular_viscos  0.1830E-04  0.1830E-04
 -----------------------------------------

 --- Diffusivity:
 -----------------------------------------------
 Scalar           Number  Min. value  Max. value
 -----------------------------------------------
 TempC                 1  0.2495E-01  0.2495E-01
 -----------------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2        2296
Smooth wall               5       33794
Rough wall                6           0
Symmetry                  4       22430
Free outlet               3        2296
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.10000E+01   0.32437E-02   0.19204E-02



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296         0.000000000E+00
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.00000E+00 0.00000E+00
   Dimensionless distance   yplus :  0.00000E+00 0.00000E+00
   Friction thermal sca.    tstar :  0.10000E+13 0.37528E+15
   Rough dim-less th. sca.  tplus :  0.74611E-12 0.74611E-12
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.11194E-04      10   0.26674E-01   0.89320E+02 0.90909E+02 
c  Velocity[X]                                      0.89299E+02 
c  Velocity[Y]                                      0.11220E-01 
c  Velocity[Z]                                      0.98882E-02 
c  Pressure     0.90575E-03    1308   0.10494E+01   0.95624E+00 0.90909E+02 
c  TempC        0.32427E+04      90   0.16993E-01   0.31958E+05 0.57362E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.10298          1.0927         0.98746         0.99051
v  Velocity[Y]             -0.5054         0.53777     5.3859e-005     6.4666e-005
v  Velocity[Z]            -0.47807         0.47286     3.5663e-006     3.3417e-005
v  ǁVelocityǁ            0.13226          1.0944         0.98818         0.99078
v  Pressure               0.091729          106.32          53.109          53.157
v  TempC                    58.814          318.18          293.23          296.58
v  CourantNb                     0               0               0               0
v  FourierNb              0.014201         0.90303         0.10864        0.071461
v  total_pressure      1.0133e+005     1.0143e+005     1.0138e+005     1.0138e+005
v  Local Time Step           0.011           0.011           0.011           0.011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014201         0.90303         0.10864        0.071461


 TIME FOR THE TIME STEP                1:        0.23259E+02

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


 INSTANT    0.200000000E-01   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447989E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.39953E-01 0.15630E+00
   Friction velocity        uk    :  0.39953E-01 0.15630E+00
   Dimensionless distance   yplus :  0.26255E+01 0.13458E+02
   Friction thermal sca.    tstar :  0.10173E+02 0.57958E+02
   Rough dim-less th. sca.  tplus :  0.19589E+01 0.10041E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34032E-01      22   0.70885E-02   0.43038E+00 0.15372E+02 
c  Velocity[X]                                      0.32302E+00 
c  Velocity[Y]                                      0.53727E-01 
c  Velocity[Z]                                      0.53638E-01 
c  Pressure     0.93110E-03     952   0.52397E-01   0.22197E+01 0.39722E+03 
c  TempC        0.10400E+05      22   0.42330E-02   0.55885E+04 0.56696E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00042357                          2605


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              0.5464          1.1441         0.99348         0.99705
v  Velocity[Y]            -0.35019         0.36165     -0.00069134     -0.00067531
v  Velocity[Z]            -0.31176         0.30815     -0.00027221     -0.00017235
v  ǁVelocityǁ            0.59715          1.1445         0.99386         0.99719
v  Pressure               -0.36534          3.2714          1.1344          1.1312
v  TempC                    37.712          324.08          292.06           295.9
v  CourantNb                     1          2.3609          1.0006          1.0002
v  FourierNb             0.0054356         0.10198        0.021012        0.016485
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0083195       0.0023323       0.0030797


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.4027          1.0216          1.0167


 TIME FOR THE TIME STEP                2:        0.19478E+02

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


 INSTANT    0.300000000E-01   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471448004E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.66201E-01 0.14828E+00
   Friction velocity        uk    :  0.66201E-01 0.14828E+00
   Dimensionless distance   yplus :  0.49873E+01 0.13633E+02
   Friction thermal sca.    tstar :  0.38032E+01 0.62293E+02
   Rough dim-less th. sca.  tplus :  0.37211E+01 0.10172E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34519E-01      22   0.84792E-02   0.97309E-01 0.75367E+01 
c  Velocity[X]                                      0.61976E-01 
c  Velocity[Y]                                      0.18044E-01 
c  Velocity[Z]                                      0.17289E-01 
c  Pressure     0.27208E-03     973   0.37139E-01   0.76608E+00 0.30794E+04 
c  TempC        0.10390E+05      22   0.55517E-02   0.48369E+04 0.52366E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step       0.0004446                          2228


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.52868          1.1795         0.99387         0.99733
v  Velocity[Y]            -0.20372         0.20106     -0.00075023     -0.00066877
v  Velocity[Z]             -0.1703         0.17335     -0.00042343     -0.00021423
v  ǁVelocityǁ            0.54039          1.1799         0.99417         0.99744
v  Pressure               -0.24054          0.6776         0.14212         0.14192
v  TempC                    22.485          339.85          290.97          295.22
v  CourantNb               0.91871          2.2492          1.0005          1.0002
v  FourierNb             0.0054571         0.10708        0.020915         0.01646
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082487       0.0023243       0.0030768


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95406           2.291          1.0214          1.0166


 TIME FOR THE TIME STEP                3:        0.24056E+02

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


 INSTANT    0.400000000E-01   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.68183E-01 0.14819E+00
   Friction velocity        uk    :  0.68183E-01 0.14819E+00
   Dimensionless distance   yplus :  0.40500E+01 0.13670E+02
   Friction thermal sca.    tstar :  0.61018E+00 0.70550E+02
   Rough dim-less th. sca.  tplus :  0.30217E+01 0.10200E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34339E-01      21   0.86737E-02   0.36453E-01 0.45727E+01 
c  Velocity[X]                                      0.22227E-01 
c  Velocity[Y]                                      0.72302E-02 
c  Velocity[Z]                                      0.69956E-02 
c  Pressure     0.18546E-03     879   0.16529E-01   0.51215E+00 0.14140E+03 
c  TempC        0.10380E+05      22   0.61831E-02   0.47107E+04 0.51157E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044191                          2220


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.51113          1.2143         0.99385         0.99754
v  Velocity[Y]            -0.16172         0.15383     -0.00076932     -0.00062931
v  Velocity[Z]            -0.16433          0.1645     -0.00048658     -0.00024487
v  ǁVelocityǁ            0.51793          1.2143         0.99417         0.99766
v  Pressure               -0.19214         0.56645         0.22115         0.22124
v  TempC                    22.561          351.45          289.92          294.52
v  CourantNb               0.91958          2.2629          1.0005          1.0002
v  FourierNb             0.0054525         0.10451        0.020938        0.016465
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082458       0.0023261       0.0030767


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95517          2.3047          1.0214          1.0166


 TIME FOR THE TIME STEP                4:        0.24472E+02

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


 INSTANT    0.500000000E-01   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.65107E-01 0.14801E+00
   Friction velocity        uk    :  0.65107E-01 0.14801E+00
   Dimensionless distance   yplus :  0.42512E+01 0.13701E+02
   Friction thermal sca.    tstar :  0.38973E+00 0.78754E+02
   Rough dim-less th. sca.  tplus :  0.31719E+01 0.10223E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34354E-01      21   0.94260E-02   0.21082E-01 0.34022E+01 
c  Velocity[X]                                      0.13242E-01 
c  Velocity[Y]                                      0.39446E-02 
c  Velocity[Z]                                      0.38953E-02 
c  Pressure     0.15300E-03     858   0.11908E-01   0.40800E+00 0.12652E+03 
c  TempC        0.10369E+05      22   0.64772E-02   0.45395E+04 0.49613E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044258                          2220


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.41947          1.2555         0.99369         0.99773
v  Velocity[Y]            -0.17656         0.15547     -0.00079294     -0.00060502
v  Velocity[Z]            -0.19548         0.16829     -0.00050045     -0.00027708
v  ǁVelocityǁ              0.425           1.257         0.99403         0.99787
v  Pressure               -0.17107         0.62686          0.3268         0.32689
v  TempC                    9.8961          360.87          288.92           293.8
v  CourantNb               0.92661          2.2595          1.0005          1.0002
v  FourierNb              0.005451         0.10326        0.020961         0.01647
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082591       0.0023279       0.0030764


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96576          2.3013          1.0215          1.0166


 TIME FOR THE TIME STEP                5:        0.20676E+02

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


 INSTANT    0.600000000E-01   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.62064E-01 0.14682E+00
   Friction velocity        uk    :  0.62064E-01 0.14682E+00
   Dimensionless distance   yplus :  0.37774E+01 0.13719E+02
   Friction thermal sca.    tstar : -0.16505E+01 0.87731E+02
   Rough dim-less th. sca.  tplus :  0.28183E+01 0.10236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34373E-01      20   0.96779E-02   0.16460E-01 0.29558E+01 
c  Velocity[X]                                      0.11264E-01 
c  Velocity[Y]                                      0.25632E-02 
c  Velocity[Z]                                      0.26327E-02 
c  Pressure     0.13908E-03     825   0.99477E-02   0.35688E+00 0.85750E+02 
c  TempC        0.10357E+05      22   0.64039E-02   0.44214E+04 0.48362E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044095                          2221


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.36446          1.2964          0.9934         0.99785
v  Velocity[Y]            -0.20072         0.16736     -0.00081732     -0.00059047
v  Velocity[Z]            -0.22668         0.18983     -0.00050418     -0.00031313
v  ǁVelocityǁ            0.36835          1.2973         0.99378           0.998
v  Pressure                -0.1612         0.72369         0.41823         0.41846
v  TempC                     15.26          366.65          287.95          293.06
v  CourantNb               0.95639          2.2678          1.0005          1.0002
v  FourierNb             0.0054492         0.10275        0.020981        0.016474
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082694       0.0023295       0.0030761


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9887          2.3096          1.0215          1.0166


 TIME FOR THE TIME STEP                6:        0.19512E+02

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


 INSTANT    0.700000000E-01   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.64000E-01 0.14633E+00
   Friction velocity        uk    :  0.64000E-01 0.14633E+00
   Dimensionless distance   yplus :  0.34784E+01 0.13810E+02
   Friction thermal sca.    tstar :  0.52541E+00 0.94255E+02
   Rough dim-less th. sca.  tplus :  0.25953E+01 0.10304E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34389E-01      20   0.95607E-02   0.14127E-01 0.27105E+01 
c  Velocity[X]                                      0.10331E-01 
c  Velocity[Y]                                      0.18400E-02 
c  Velocity[Z]                                      0.19551E-02 
c  Pressure     0.12998E-03     820   0.87911E-02   0.32072E+00 0.67825E+02 
c  TempC        0.10344E+05      22   0.63293E-02   0.43814E+04 0.47667E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044137                          2216


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.33881          1.3357         0.99302         0.99793
v  Velocity[Y]             -0.2203         0.17091     -0.00083444     -0.00057803
v  Velocity[Z]            -0.25453          0.2004     -0.00052394     -0.00036047
v  ǁVelocityǁ            0.34244          1.3375         0.99345         0.99809
v  Pressure               -0.14588         0.80801         0.50557         0.50595
v  TempC                    4.0482          370.05          287.01           292.3
v  CourantNb               0.93169          2.2657          1.0005          1.0002
v  FourierNb             0.0054468         0.10274        0.020999        0.016477
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082773       0.0023308       0.0030758


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96723          2.3075          1.0215          1.0166


 TIME FOR THE TIME STEP                7:        0.18955E+02

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


 INSTANT    0.800000000E-01   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447997E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.59126E-01 0.14636E+00
   Friction velocity        uk    :  0.59126E-01 0.14636E+00
   Dimensionless distance   yplus :  0.33492E+01 0.13864E+02
   Friction thermal sca.    tstar : -0.69087E+00 0.96939E+02
   Rough dim-less th. sca.  tplus :  0.24989E+01 0.10344E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34403E-01      20   0.93613E-02   0.12909E-01 0.25749E+01 
c  Velocity[X]                                      0.98553E-02 
c  Velocity[Y]                                      0.14648E-02 
c  Velocity[Z]                                      0.15885E-02 
c  Pressure     0.12258E-03     783   0.80007E-02   0.29256E+00 0.56136E+02 
c  TempC        0.10331E+05      22   0.56399E-02   0.42564E+04 0.46448E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044065                          2212


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.28318          1.3581         0.99261         0.99797
v  Velocity[Y]            -0.23419         0.18584     -0.00084887     -0.00056783
v  Velocity[Z]            -0.27772         0.21171     -0.00056233     -0.00041653
v  ǁVelocityǁ            0.28633          1.3594         0.99307         0.99815
v  Pressure               -0.13574         0.89408         0.58991         0.59038
v  TempC                   -4.3047          371.65           286.1          291.52
v  CourantNb               0.90593          2.2694          1.0005          1.0002
v  FourierNb             0.0054446         0.10285        0.021014         0.01648
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001        0.008283        0.002332       0.0030755


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94504          2.3111          1.0215          1.0166


 TIME FOR THE TIME STEP                8:        0.19292E+02

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


 INSTANT    0.900000000E-01   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447997E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60445E-01 0.14568E+00
   Friction velocity        uk    :  0.60445E-01 0.14568E+00
   Dimensionless distance   yplus :  0.27355E+01 0.13926E+02
   Friction thermal sca.    tstar : -0.97497E+00 0.96463E+02
   Rough dim-less th. sca.  tplus :  0.20410E+01 0.10391E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34417E-01      20   0.92743E-02   0.11778E-01 0.24496E+01 
c  Velocity[X]                                      0.91615E-02 
c  Velocity[Y]                                      0.12397E-02 
c  Velocity[Z]                                      0.13765E-02 
c  Pressure     0.11611E-03     772   0.73291E-02   0.26926E+00 0.47441E+02 
c  TempC        0.10316E+05      22   0.58533E-02   0.40899E+04 0.44997E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00043888                          2213


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.33845          1.3692         0.99217         0.99799
v  Velocity[Y]            -0.23978         0.19835     -0.00085921     -0.00055965
v  Velocity[Z]            -0.29867         0.22107     -0.00062639     -0.00048374
v  ǁVelocityǁ            0.34119          1.3706         0.99267         0.99818
v  Pressure               -0.12622         0.97959         0.67098         0.67157
v  TempC                   -6.8094          369.76          285.21          290.73
v  CourantNb               0.96312          2.2785          1.0005          1.0002
v  FourierNb             0.0054425           0.102        0.021027        0.016482
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082867        0.002333       0.0030751


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0015          2.3203          1.0215          1.0166


 TIME FOR THE TIME STEP                9:        0.19201E+02

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


 INSTANT    0.100000000E+00   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.61515E-01 0.14579E+00
   Friction velocity        uk    :  0.61515E-01 0.14579E+00
   Dimensionless distance   yplus :  0.33358E+01 0.13984E+02
   Friction thermal sca.    tstar : -0.60099E+01 0.94359E+02
   Rough dim-less th. sca.  tplus :  0.24889E+01 0.10434E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34430E-01      20   0.89128E-02   0.11057E-01 0.23673E+01 
c  Velocity[X]                                      0.87347E-02 
c  Velocity[Y]                                      0.10922E-02 
c  Velocity[Z]                                      0.12300E-02 
c  Pressure     0.11055E-03     770   0.68307E-02   0.25226E+00 0.40239E+02 
c  TempC        0.10301E+05      22   0.55595E-02   0.39811E+04 0.43993E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044073                          2224


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.27119          1.3713         0.99173         0.99801
v  Velocity[Y]            -0.24866          0.2122     -0.00086617      -0.0005523
v  Velocity[Z]            -0.31458         0.22319     -0.00070761     -0.00055804
v  ǁVelocityǁ            0.27779          1.3732         0.99226         0.99821
v  Pressure               -0.11684            1.06          0.7476         0.74825
v  TempC                   -1.3803          372.42          284.34          289.92
v  CourantNb               0.92827          2.2689          1.0005          1.0002
v  FourierNb             0.0054404          0.1027         0.02104        0.016484
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082889       0.0023339       0.0030748


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96294          2.3107          1.0215          1.0166


 TIME FOR THE TIME STEP               10:        0.18160E+02

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


 INSTANT    0.110000000E+00   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54059E-01 0.14536E+00
   Friction velocity        uk    :  0.54059E-01 0.14536E+00
   Dimensionless distance   yplus :  0.30166E+01 0.14043E+02
   Friction thermal sca.    tstar : -0.53247E+01 0.91300E+02
   Rough dim-less th. sca.  tplus :  0.22508E+01 0.10478E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34442E-01      20   0.86939E-02   0.10136E-01 0.22627E+01 
c  Velocity[X]                                      0.80434E-02 
c  Velocity[Y]                                      0.98067E-03 
c  Velocity[Z]                                      0.11119E-02 
c  Pressure     0.10496E-03     754   0.63182E-02   0.23550E+00 0.34842E+02 
c  TempC        0.10286E+05      22   0.56157E-02   0.38435E+04 0.42794E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044132                          2233


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               0.226          1.3647         0.99129         0.99802
v  Velocity[Y]            -0.24852         0.22298     -0.00086743     -0.00054439
v  Velocity[Z]            -0.33114         0.22538     -0.00080665     -0.00063947
v  ǁVelocityǁ             0.2352           1.365         0.99183         0.99824
v  Pressure               -0.10958          1.1311         0.82041         0.82115
v  TempC                    4.6598          375.64          283.49           289.1
v  CourantNb               0.92201          2.2659          1.0005          1.0002
v  FourierNb             0.0054384         0.10287        0.021053        0.016486
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082903       0.0023348       0.0030745


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96014          2.3077          1.0215          1.0167


 TIME FOR THE TIME STEP               11:        0.17930E+02

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


 INSTANT    0.120000000E+00   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.46568E-01 0.14562E+00
   Friction velocity        uk    :  0.46568E-01 0.14562E+00
   Dimensionless distance   yplus :  0.34601E+01 0.14095E+02
   Friction thermal sca.    tstar : -0.37377E+01 0.89844E+02
   Rough dim-less th. sca.  tplus :  0.25816E+01 0.10517E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34455E-01      20   0.85444E-02   0.93331E-02 0.21691E+01 
c  Velocity[X]                                      0.74564E-02 
c  Velocity[Y]                                      0.87598E-03 
c  Velocity[Z]                                      0.10007E-02 
c  Pressure     0.10054E-03     752   0.59187E-02   0.22297E+00 0.30268E+02 
c  TempC        0.10270E+05      22   0.57951E-02   0.37757E+04 0.42188E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044219                          2236


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.17886          1.3675         0.99086         0.99804
v  Velocity[Y]            -0.24733         0.23922     -0.00086849     -0.00053849
v  Velocity[Z]              -0.346         0.23277     -0.00091516     -0.00072532
v  ǁVelocityǁ            0.19065           1.368         0.99142         0.99826
v  Pressure               -0.10085          1.1998         0.88896         0.88973
v  TempC                    6.4683          376.49          282.65          288.27
v  CourantNb               0.91343          2.2615          1.0005          1.0002
v  FourierNb             0.0054366         0.10327        0.021065        0.016489
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082909       0.0023357       0.0030742


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96958          2.3033          1.0216          1.0167


 TIME FOR THE TIME STEP               12:        0.18133E+02

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


 INSTANT    0.130000000E+00   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.40603E-01 0.14586E+00
   Friction velocity        uk    :  0.40603E-01 0.14586E+00
   Dimensionless distance   yplus :  0.31311E+01 0.14127E+02
   Friction thermal sca.    tstar : -0.24251E+01 0.89148E+02
   Rough dim-less th. sca.  tplus :  0.23362E+01 0.10540E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34468E-01      20   0.86222E-02   0.94787E-02 0.21766E+01 
c  Velocity[X]                                      0.76425E-02 
c  Velocity[Y]                                      0.86715E-03 
c  Velocity[Z]                                      0.96904E-03 
c  Pressure     0.97260E-04     752   0.56144E-02   0.21413E+00 0.26178E+02 
c  TempC        0.10253E+05      22   0.58351E-02   0.37208E+04 0.41691E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044276                          2234


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.16181           1.385         0.99042         0.99805
v  Velocity[Y]            -0.25418         0.26136      -0.0008698     -0.00053363
v  Velocity[Z]            -0.35932         0.23868      -0.0010274     -0.00081321
v  ǁVelocityǁ            0.16724          1.3906           0.991         0.99828
v  Pressure              -0.095121          1.2627         0.95248          0.9533
v  TempC                    15.346          378.31          281.82          287.42
v  CourantNb               0.87696          2.2586          1.0005          1.0002
v  FourierNb             0.0054346         0.10477        0.021078        0.016491
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082897       0.0023367       0.0030739


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93873          2.3003          1.0216          1.0167


 TIME FOR THE TIME STEP               13:        0.20154E+02

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


 INSTANT    0.140000000E+00   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48039E-01 0.14573E+00
   Friction velocity        uk    :  0.48039E-01 0.14573E+00
   Dimensionless distance   yplus :  0.28957E+01 0.14169E+02
   Friction thermal sca.    tstar : -0.75244E+00 0.88170E+02
   Rough dim-less th. sca.  tplus :  0.21605E+01 0.10572E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34481E-01      20   0.87802E-02   0.91267E-02 0.21350E+01 
c  Velocity[X]                                      0.73695E-02 
c  Velocity[Y]                                      0.81545E-03 
c  Velocity[Z]                                      0.94175E-03 
c  Pressure     0.94311E-04     753   0.53153E-02   0.20667E+00 0.23322E+02 
c  TempC        0.10236E+05      22   0.58360E-02   0.36498E+04 0.41140E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044379                          2216


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20443          1.4184         0.98999         0.99806
v  Velocity[Y]            -0.25515         0.28016     -0.00087054      -0.0005298
v  Velocity[Z]            -0.37104         0.23169      -0.0011407     -0.00090186
v  ǁVelocityǁ            0.20698          1.4244         0.99058         0.99829
v  Pressure              -0.093828          1.3236          1.0127          1.0135
v  TempC                    16.283          379.21             281          286.57
v  CourantNb                     1          2.2533          1.0005          1.0002
v  FourierNb             0.0054327         0.10524        0.021091        0.016493
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082889       0.0023376       0.0030736


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2951          1.0216          1.0167


 TIME FOR THE TIME STEP               14:        0.18645E+02

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


 INSTANT    0.150000000E+00   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52202E-01 0.14571E+00
   Friction velocity        uk    :  0.52202E-01 0.14571E+00
   Dimensionless distance   yplus :  0.34155E+01 0.14225E+02
   Friction thermal sca.    tstar :  0.50373E+00 0.89201E+02
   Rough dim-less th. sca.  tplus :  0.25483E+01 0.10614E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34493E-01      20   0.84565E-02   0.91944E-02 0.21354E+01 
c  Velocity[X]                                      0.74714E-02 
c  Velocity[Y]                                      0.80444E-03 
c  Velocity[Z]                                      0.91851E-03 
c  Pressure     0.95680E-04     771   0.52799E-02   0.20929E+00 0.21392E+02 
c  TempC        0.10218E+05      22   0.59992E-02   0.35990E+04 0.40795E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044548                          2208


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22285           1.435         0.98957         0.99807
v  Velocity[Y]            -0.26374         0.29588     -0.00087246     -0.00052738
v  Velocity[Z]            -0.37844         0.23262      -0.0012535     -0.00099128
v  ǁVelocityǁ            0.22534          1.4381         0.99017         0.99831
v  Pressure              -0.087573          1.3837           1.071          1.0719
v  TempC                    18.747          378.45          280.19           285.7
v  CourantNb               0.96733          2.2447          1.0005          1.0002
v  FourierNb             0.0054308         0.10435        0.021103        0.016496
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082878       0.0023385       0.0030733


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9999          2.2865          1.0216          1.0167


 TIME FOR THE TIME STEP               15:        0.18220E+02

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


 INSTANT    0.160000000E+00   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48624E-01 0.14555E+00
   Friction velocity        uk    :  0.48624E-01 0.14555E+00
   Dimensionless distance   yplus :  0.30970E+01 0.14278E+02
   Friction thermal sca.    tstar :  0.10279E+01 0.90910E+02
   Rough dim-less th. sca.  tplus :  0.23107E+01 0.10653E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34506E-01      20   0.85041E-02   0.87642E-02 0.20855E+01 
c  Velocity[X]                                      0.70702E-02 
c  Velocity[Y]                                      0.79009E-03 
c  Velocity[Z]                                      0.90384E-03 
c  Pressure     0.92031E-04     752   0.50868E-02   0.20095E+00 0.19817E+02 
c  TempC        0.10201E+05      22   0.59081E-02   0.35566E+04 0.40566E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044554                          2194


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22596          1.4402         0.98914         0.99808
v  Velocity[Y]            -0.26553         0.30769     -0.00087188     -0.00052524
v  Velocity[Z]            -0.38752         0.22198      -0.0013728      -0.0010833
v  ǁVelocityǁ            0.23026          1.4433         0.98976         0.99833
v  Pressure              -0.080636          1.4402           1.128          1.1289
v  TempC                    17.293           376.5          279.38          284.84
v  CourantNb                     1          2.2445          1.0005          1.0002
v  FourierNb             0.0054289         0.10475        0.021115        0.016498
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082868       0.0023393        0.003073


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2863          1.0216          1.0167


 TIME FOR THE TIME STEP               16:        0.18072E+02

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


 INSTANT    0.170000000E+00   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.46936E-01 0.14501E+00
   Friction velocity        uk    :  0.46936E-01 0.14501E+00
   Dimensionless distance   yplus :  0.28616E+01 0.14308E+02
   Friction thermal sca.    tstar :  0.63895E+00 0.91574E+02
   Rough dim-less th. sca.  tplus :  0.21351E+01 0.10675E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34518E-01      20   0.86536E-02   0.86782E-02 0.20691E+01 
c  Velocity[X]                                      0.70179E-02 
c  Velocity[Y]                                      0.76998E-03 
c  Velocity[Z]                                      0.89028E-03 
c  Pressure     0.89111E-04     748   0.48221E-02   0.19445E+00 0.17375E+02 
c  TempC        0.10183E+05      22   0.59719E-02   0.34780E+04 0.40097E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044668                          2181


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22666          1.4412         0.98873         0.99809
v  Velocity[Y]             -0.2654           0.318     -0.00087158     -0.00052179
v  Velocity[Z]            -0.39636         0.23121      -0.0014909      -0.0011747
v  ǁVelocityǁ            0.22994          1.4444         0.98935         0.99834
v  Pressure              -0.082264            1.49          1.1802          1.1812
v  TempC                    18.887          353.89          278.58          283.97
v  CourantNb               0.99149          2.2387          1.0005          1.0002
v  FourierNb             0.0054268         0.10513        0.021128          0.0165
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082863       0.0023403       0.0030727


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2805          1.0216          1.0167


 TIME FOR THE TIME STEP               17:        0.18685E+02

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


 INSTANT    0.180000000E+00   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55117E-01 0.14491E+00
   Friction velocity        uk    :  0.55117E-01 0.14491E+00
   Dimensionless distance   yplus :  0.32942E+01 0.14322E+02
   Friction thermal sca.    tstar :  0.65879E+00 0.92868E+02
   Rough dim-less th. sca.  tplus :  0.24578E+01 0.10686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34530E-01      20   0.86129E-02   0.91937E-02 0.21215E+01 
c  Velocity[X]                                      0.75061E-02 
c  Velocity[Y]                                      0.78903E-03 
c  Velocity[Z]                                      0.89856E-03 
c  Pressure     0.94689E-04     752   0.50509E-02   0.20696E+00 0.17085E+02 
c  TempC        0.10165E+05      22   0.58756E-02   0.34420E+04 0.39949E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044685                          2169


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22565          1.4534         0.98831          0.9981
v  Velocity[Y]            -0.26828         0.32932     -0.00086938     -0.00051951
v  Velocity[Z]            -0.40377         0.23698      -0.0016034      -0.0012632
v  ǁVelocityǁ            0.22769          1.4585         0.98894         0.99835
v  Pressure              -0.071789          1.5441          1.2339          1.2349
v  TempC                    15.914          349.42          277.79           283.1
v  CourantNb                     1          2.2379          1.0005          1.0002
v  FourierNb             0.0054247         0.10486         0.02114        0.016503
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082847       0.0023411       0.0030724


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2797          1.0216          1.0167


 TIME FOR THE TIME STEP               18:        0.18130E+02

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


 INSTANT    0.190000000E+00   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54093E-01 0.14493E+00
   Friction velocity        uk    :  0.54093E-01 0.14493E+00
   Dimensionless distance   yplus :  0.29795E+01 0.14352E+02
   Friction thermal sca.    tstar :  0.71809E+00 0.94362E+02
   Rough dim-less th. sca.  tplus :  0.22230E+01 0.10708E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34542E-01      20   0.84228E-02   0.88248E-02 0.20771E+01 
c  Velocity[X]                                      0.71894E-02 
c  Velocity[Y]                                      0.77476E-03 
c  Velocity[Z]                                      0.86060E-03 
c  Pressure     0.87716E-04     768   0.46197E-02   0.19202E+00 0.15257E+02 
c  TempC        0.10147E+05      22   0.58741E-02   0.33624E+04 0.39497E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00044823                          2146


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20311          1.4571          0.9879         0.99811
v  Velocity[Y]            -0.26501         0.33992     -0.00086705     -0.00051748
v  Velocity[Z]            -0.41042         0.22808      -0.0017159      -0.0013517
v  ǁVelocityǁ            0.20373          1.4606         0.98854         0.99837
v  Pressure               -0.07257          1.5966          1.2839          1.2849
v  TempC                    13.995          354.59             277          282.22
v  CourantNb                     1           2.231          1.0005          1.0002
v  FourierNb             0.0054225         0.10505        0.021152        0.016505
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082833        0.002342       0.0030721


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2728          1.0216          1.0167


 TIME FOR THE TIME STEP               19:        0.17980E+02

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


 INSTANT    0.200000000E+00   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53813E-01 0.14438E+00
   Friction velocity        uk    :  0.53813E-01 0.14438E+00
   Dimensionless distance   yplus :  0.32375E+01 0.14395E+02
   Friction thermal sca.    tstar : -0.32719E+00 0.92681E+02
   Rough dim-less th. sca.  tplus :  0.24155E+01 0.10740E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34555E-01      20   0.82402E-02   0.85038E-02 0.20353E+01 
c  Velocity[X]                                      0.69186E-02 
c  Velocity[Y]                                      0.74501E-03 
c  Velocity[Z]                                      0.84016E-03 
c  Pressure     0.89731E-04     786   0.46915E-02   0.19667E+00 0.14509E+02 
c  TempC        0.10128E+05      22   0.58648E-02   0.33098E+04 0.39260E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045001                          2117


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.19016          1.4546         0.98749         0.99812
v  Velocity[Y]            -0.27331         0.34915     -0.00086617     -0.00051726
v  Velocity[Z]            -0.41547         0.22773      -0.0018293      -0.0014403
v  ǁVelocityǁ            0.19036          1.4714         0.98814         0.99838
v  Pressure              -0.059182          1.6419          1.3332          1.3342
v  TempC                    8.9322           364.5          276.21          281.35
v  CourantNb                     1          2.2222          1.0005          1.0002
v  FourierNb             0.0054205          0.1047        0.021165        0.016508
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082824       0.0023429       0.0030718


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054           2.264          1.0216          1.0167


 TIME FOR THE TIME STEP               20:        0.18269E+02

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


 INSTANT    0.210000000E+00   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52094E-01 0.14473E+00
   Friction velocity        uk    :  0.52094E-01 0.14473E+00
   Dimensionless distance   yplus :  0.31945E+01 0.14440E+02
   Friction thermal sca.    tstar : -0.19891E+01 0.92988E+02
   Rough dim-less th. sca.  tplus :  0.23835E+01 0.10774E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34567E-01      20   0.84096E-02   0.82907E-02 0.20054E+01 
c  Velocity[X]                                      0.67194E-02 
c  Velocity[Y]                                      0.73360E-03 
c  Velocity[Z]                                      0.83766E-03 
c  Pressure     0.83015E-04     750   0.41803E-02   0.18193E+00 0.12496E+02 
c  TempC        0.10110E+05      22   0.58994E-02   0.32665E+04 0.39104E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045007                          2110


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.18924          1.4765         0.98709         0.99813
v  Velocity[Y]            -0.28266         0.35311     -0.00086214     -0.00051461
v  Velocity[Z]            -0.42451         0.21896      -0.0019425      -0.0015282
v  ǁVelocityǁ            0.18996          1.4808         0.98774          0.9984
v  Pressure              -0.064918          1.6902           1.377          1.3781
v  TempC                    17.597          369.16          275.42          280.48
v  CourantNb                     1          2.2219          1.0005          1.0002
v  FourierNb             0.0054184         0.10501        0.021177         0.01651
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082812       0.0023438       0.0030716


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2637          1.0217          1.0167


 TIME FOR THE TIME STEP               21:        0.23360E+02

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


 INSTANT    0.220000000E+00   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51903E-01 0.14607E+00
   Friction velocity        uk    :  0.51903E-01 0.14607E+00
   Dimensionless distance   yplus :  0.28444E+01 0.14473E+02
   Friction thermal sca.    tstar : -0.43225E+00 0.91866E+02
   Rough dim-less th. sca.  tplus :  0.21223E+01 0.10799E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34579E-01      20   0.84061E-02   0.85070E-02 0.20296E+01 
c  Velocity[X]                                      0.69349E-02 
c  Velocity[Y]                                      0.74063E-03 
c  Velocity[Z]                                      0.83145E-03 
c  Pressure     0.88549E-04     754   0.45192E-02   0.19463E+00 0.12391E+02 
c  TempC        0.10091E+05      22   0.58751E-02   0.32149E+04 0.38863E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045106                          2095


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.24633          1.4916         0.98669         0.99814
v  Velocity[Y]            -0.27718         0.35747     -0.00086325     -0.00051438
v  Velocity[Z]             -0.4278         0.22335      -0.0020515      -0.0016138
v  ǁVelocityǁ             0.2482          1.4986         0.98735         0.99841
v  Pressure               -0.06246           1.737          1.4219           1.423
v  TempC                    19.982          371.97          274.64          279.61
v  CourantNb                     1           2.217          1.0005          1.0002
v  FourierNb             0.0054164         0.10522         0.02119        0.016513
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082797       0.0023447       0.0030713


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2588          1.0217          1.0167


 TIME FOR THE TIME STEP               22:        0.21882E+02

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


 INSTANT    0.230000000E+00   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49549E-01 0.14761E+00
   Friction velocity        uk    :  0.49549E-01 0.14761E+00
   Dimensionless distance   yplus :  0.32127E+01 0.14467E+02
   Friction thermal sca.    tstar :  0.44817E+00 0.90587E+02
   Rough dim-less th. sca.  tplus :  0.23970E+01 0.10794E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34591E-01      20   0.82676E-02   0.85853E-02 0.20316E+01 
c  Velocity[X]                                      0.70158E-02 
c  Velocity[Y]                                      0.73608E-03 
c  Velocity[Z]                                      0.83340E-03 
c  Pressure     0.86886E-04     770   0.44494E-02   0.19125E+00 0.12125E+02 
c  TempC        0.10073E+05      22   0.59958E-02   0.31716E+04 0.38680E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045026                          2086


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.24345          1.5084         0.98629         0.99814
v  Velocity[Y]            -0.28069         0.36185     -0.00085889     -0.00051169
v  Velocity[Z]            -0.43425         0.22506      -0.0021589       -0.001698
v  ǁVelocityǁ            0.24977          1.5162         0.98696         0.99842
v  Pressure              -0.063018          1.7767          1.4672          1.4684
v  TempC                    15.124           374.3          273.86          278.74
v  CourantNb                     1          2.2209          1.0005          1.0002
v  FourierNb             0.0054143         0.10564        0.021202        0.016516
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082773       0.0023456       0.0030711


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2627          1.0217          1.0167


 TIME FOR THE TIME STEP               23:        0.22314E+02

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


 INSTANT    0.240000000E+00   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.59505E-01 0.14868E+00
   Friction velocity        uk    :  0.59505E-01 0.14868E+00
   Dimensionless distance   yplus :  0.28987E+01 0.14483E+02
   Friction thermal sca.    tstar :  0.94416E+00 0.89036E+02
   Rough dim-less th. sca.  tplus :  0.21627E+01 0.10806E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34603E-01      20   0.82167E-02   0.80740E-02 0.19713E+01 
c  Velocity[X]                                      0.65392E-02 
c  Velocity[Y]                                      0.71638E-03 
c  Velocity[Z]                                      0.81847E-03 
c  Pressure     0.87612E-04     751   0.45399E-02   0.19312E+00 0.12165E+02 
c  TempC        0.10054E+05      22   0.60057E-02   0.31646E+04 0.38806E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045072                          2076


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.26154          1.5276          0.9859         0.99815
v  Velocity[Y]            -0.28161         0.36712     -0.00085712     -0.00051142
v  Velocity[Z]            -0.43442         0.22266      -0.0022672      -0.0017824
v  ǁVelocityǁ            0.26594          1.5353         0.98658         0.99844
v  Pressure              -0.045641          1.8261          1.5142          1.5154
v  TempC                   -5.2023          375.98          273.08          277.88
v  CourantNb                     1          2.2187          1.0005          1.0002
v  FourierNb             0.0054123          0.1056        0.021214        0.016518
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082759       0.0023464       0.0030708


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2604          1.0217          1.0167


 TIME FOR THE TIME STEP               24:        0.20370E+02

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


 INSTANT    0.250000000E+00   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.58048E-01 0.14982E+00
   Friction velocity        uk    :  0.58048E-01 0.14982E+00
   Dimensionless distance   yplus :  0.33277E+01 0.14505E+02
   Friction thermal sca.    tstar :  0.58300E+00 0.84358E+02
   Rough dim-less th. sca.  tplus :  0.24828E+01 0.10822E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         25, Physical time    0.25000E+00


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
 End writing


 Time for restart files:    0.18502E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34616E-01      20   0.83448E-02   0.81806E-02 0.19782E+01 
c  Velocity[X]                                      0.66679E-02 
c  Velocity[Y]                                      0.72112E-03 
c  Velocity[Z]                                      0.79151E-03 
c  Pressure     0.80666E-04     765   0.38818E-02   0.17806E+00 0.95087E+01 
c  TempC        0.10036E+05      22   0.58811E-02   0.31139E+04 0.38550E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045234                          2058


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.26067            1.54         0.98551         0.99816
v  Velocity[Y]            -0.29106         0.37161     -0.00085608     -0.00051016
v  Velocity[Z]            -0.43371          0.2087      -0.0023688      -0.0018633
v  ǁVelocityǁ            0.26395          1.5485          0.9862         0.99845
v  Pressure              -0.052523          1.8659          1.5518           1.553
v  TempC                   -14.035          375.26           272.3          277.01
v  CourantNb                     1          2.2107          1.0005          1.0002
v  FourierNb             0.0054103         0.10562        0.021227        0.016521
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001        0.008277       0.0023473       0.0030706


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2525          1.0217          1.0167


 TIME FOR THE TIME STEP               25:        0.21975E+02

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


 INSTANT    0.260000000E+00   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57100E-01 0.15067E+00
   Friction velocity        uk    :  0.57100E-01 0.15067E+00
   Dimensionless distance   yplus :  0.31266E+01 0.14547E+02
   Friction thermal sca.    tstar : -0.20511E+00 0.82138E+02
   Rough dim-less th. sca.  tplus :  0.23328E+01 0.10854E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34628E-01      20   0.81490E-02   0.83221E-02 0.19950E+01 
c  Velocity[X]                                      0.67968E-02 
c  Velocity[Y]                                      0.71957E-03 
c  Velocity[Z]                                      0.80573E-03 
c  Pressure     0.86684E-04     770   0.43246E-02   0.19200E+00 0.10049E+02 
c  TempC        0.10017E+05      22   0.58631E-02   0.30443E+04 0.38159E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045117                          2047


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.24506          1.5653         0.98512         0.99817
v  Velocity[Y]             -0.2917         0.37478     -0.00085671     -0.00051059
v  Velocity[Z]            -0.43733         0.21413      -0.0024667       -0.001942
v  ǁVelocityǁ            0.24661          1.5735         0.98581         0.99846
v  Pressure              -0.050724          1.9058          1.5926          1.5939
v  TempC                   -20.653          373.02          271.52          276.15
v  CourantNb               0.99978          2.2164          1.0005          1.0002
v  FourierNb             0.0054084          0.1058        0.021239        0.016524
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082771       0.0023482       0.0030703


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2582          1.0217          1.0167


 TIME FOR THE TIME STEP               26:        0.19420E+02

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


 INSTANT    0.270000000E+00   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.56928E-01 0.15207E+00
   Friction velocity        uk    :  0.56928E-01 0.15207E+00
   Dimensionless distance   yplus :  0.27370E+01 0.14568E+02
   Friction thermal sca.    tstar :  0.93367E+00 0.80607E+02
   Rough dim-less th. sca.  tplus :  0.20421E+01 0.10869E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34640E-01      20   0.81114E-02   0.81774E-02 0.19732E+01 
c  Velocity[X]                                      0.66636E-02 
c  Velocity[Y]                                      0.71279E-03 
c  Velocity[Z]                                      0.80099E-03 
c  Pressure     0.83838E-04     772   0.41290E-02   0.18612E+00 0.95368E+01 
c  TempC        0.99985E+04      22   0.60401E-02   0.30401E+04 0.38270E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045219                          2038


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              0.2343          1.5784         0.98473         0.99817
v  Velocity[Y]            -0.28705         0.37967      -0.0008542     -0.00050918
v  Velocity[Z]            -0.44585         0.21725      -0.0025647      -0.0020203
v  ǁVelocityǁ             0.2371          1.5875         0.98543         0.99847
v  Pressure              -0.050032          1.9453          1.6323          1.6336
v  TempC                   -19.422          349.23          270.75          275.29
v  CourantNb                     1          2.2115          1.0005          1.0001
v  FourierNb             0.0054065          0.1059        0.021252        0.016526
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082762       0.0023491       0.0030701


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2532          1.0217          1.0167


 TIME FOR THE TIME STEP               27:        0.20219E+02

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


 INSTANT    0.280000000E+00   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55173E-01 0.15301E+00
   Friction velocity        uk    :  0.55173E-01 0.15301E+00
   Dimensionless distance   yplus :  0.31967E+01 0.14580E+02
   Friction thermal sca.    tstar :  0.61151E+00 0.79407E+02
   Rough dim-less th. sca.  tplus :  0.23851E+01 0.10879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34652E-01      20   0.80177E-02   0.79011E-02 0.19370E+01 
c  Velocity[X]                                      0.64293E-02 
c  Velocity[Y]                                      0.70192E-03 
c  Velocity[Z]                                      0.76991E-03 
c  Pressure     0.83920E-04     770   0.41498E-02   0.18657E+00 0.96309E+01 
c  TempC        0.99797E+04      22   0.60770E-02   0.30180E+04 0.38232E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045383                          2021


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21422           1.593         0.98435         0.99818
v  Velocity[Y]            -0.30213         0.38506     -0.00085302     -0.00050955
v  Velocity[Z]            -0.44983          0.2186      -0.0026624      -0.0020971
v  ǁVelocityǁ            0.21532          1.6074         0.98506         0.99849
v  Pressure              -0.036486           1.986          1.6734          1.6747
v  TempC                   -2.9287          340.58          269.97          274.43
v  CourantNb                     1          2.2035          1.0005          1.0001
v  FourierNb             0.0054047         0.10573        0.021264        0.016529
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082747         0.00235       0.0030699


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2452          1.0217          1.0167


 TIME FOR THE TIME STEP               28:        0.20301E+02

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


 INSTANT    0.290000000E+00   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50915E-01 0.15389E+00
   Friction velocity        uk    :  0.50915E-01 0.15389E+00
   Dimensionless distance   yplus :  0.28392E+01 0.14573E+02
   Friction thermal sca.    tstar :  0.10394E+01 0.79475E+02
   Rough dim-less th. sca.  tplus :  0.21183E+01 0.10873E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34664E-01      20   0.81885E-02   0.78528E-02 0.19286E+01 
c  Velocity[X]                                      0.64031E-02 
c  Velocity[Y]                                      0.68853E-03 
c  Velocity[Z]                                      0.76116E-03 
c  Pressure     0.78890E-04     751   0.36663E-02   0.17553E+00 0.77697E+01 
c  TempC        0.99610E+04      22   0.58934E-02   0.29662E+04 0.37921E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045265                          2006


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21038          1.6054         0.98397         0.99819
v  Velocity[Y]            -0.31369         0.38966     -0.00084991     -0.00050727
v  Velocity[Z]            -0.45532         0.21831      -0.0027589       -0.002173
v  ǁVelocityǁ            0.21045          1.6211         0.98469          0.9985
v  Pressure              -0.041921          2.0225          1.7072          1.7086
v  TempC                   -1.2478          349.48           269.2          273.57
v  CourantNb                     1          2.2092          1.0005          1.0001
v  FourierNb             0.0054028          0.1057        0.021277        0.016532
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082743       0.0023509       0.0030696


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054           2.251          1.0217          1.0167


 TIME FOR THE TIME STEP               29:        0.19294E+02

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


 INSTANT    0.300000000E+00   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.47992E-01 0.15459E+00
   Friction velocity        uk    :  0.47992E-01 0.15459E+00
   Dimensionless distance   yplus :  0.32292E+01 0.14596E+02
   Friction thermal sca.    tstar :  0.78195E+00 0.78122E+02
   Rough dim-less th. sca.  tplus :  0.24093E+01 0.10890E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34676E-01      20   0.81318E-02   0.81539E-02 0.19614E+01 
c  Velocity[X]                                      0.66613E-02 
c  Velocity[Y]                                      0.70914E-03 
c  Velocity[Z]                                      0.78341E-03 
c  Pressure     0.83596E-04     720   0.39826E-02   0.18658E+00 0.78626E+01 
c  TempC        0.99423E+04      22   0.59358E-02   0.29122E+04 0.37608E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045273                          1999


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.23733          1.6264         0.98359         0.99819
v  Velocity[Y]            -0.31483         0.39458     -0.00084955     -0.00050811
v  Velocity[Z]            -0.44852         0.21703      -0.0028504      -0.0022454
v  ǁVelocityǁ            0.24531          1.6354         0.98432         0.99851
v  Pressure              -0.041101          2.0571          1.7422          1.7435
v  TempC                    6.2872          358.23          268.43          272.71
v  CourantNb                     1          2.2088          1.0005          1.0001
v  FourierNb             0.0054011          0.1062        0.021289        0.016535
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082735       0.0023518       0.0030694


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2506          1.0217          1.0167


 TIME FOR THE TIME STEP               30:        0.18649E+02

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


 INSTANT    0.310000000E+00   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55254E-01 0.15569E+00
   Friction velocity        uk    :  0.55254E-01 0.15569E+00
   Dimensionless distance   yplus :  0.30894E+01 0.14608E+02
   Friction thermal sca.    tstar :  0.77387E+00 0.78413E+02
   Rough dim-less th. sca.  tplus :  0.23050E+01 0.10899E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34688E-01      20   0.79964E-02   0.79367E-02 0.19343E+01 
c  Velocity[X]                                      0.64806E-02 
c  Velocity[Y]                                      0.69317E-03 
c  Velocity[Z]                                      0.76294E-03 
c  Pressure     0.80933E-04     734   0.38371E-02   0.18084E+00 0.77067E+01 
c  TempC        0.99235E+04      22   0.58816E-02   0.28886E+04 0.37523E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045431                          1977


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.23313          1.6315         0.98322          0.9982
v  Velocity[Y]            -0.32219         0.39717     -0.00084544     -0.00050689
v  Velocity[Z]            -0.45654         0.20423      -0.0029441      -0.0023191
v  ǁVelocityǁ            0.23968          1.6496         0.98395         0.99852
v  Pressure              -0.046604          2.0953          1.7771          1.7784
v  TempC                    5.6032          362.09          267.65          271.86
v  CourantNb               0.98029          2.2012          1.0005          1.0001
v  FourierNb             0.0053993         0.10618        0.021301        0.016537
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082732       0.0023526       0.0030692


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2429          1.0218          1.0167


 TIME FOR THE TIME STEP               31:        0.19135E+02

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


 INSTANT    0.320000000E+00   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54241E-01 0.15613E+00
   Friction velocity        uk    :  0.54241E-01 0.15613E+00
   Dimensionless distance   yplus :  0.27363E+01 0.14617E+02
   Friction thermal sca.    tstar :  0.45984E+00 0.78044E+02
   Rough dim-less th. sca.  tplus :  0.20416E+01 0.10906E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34700E-01      20   0.79259E-02   0.78692E-02 0.19238E+01 
c  Velocity[X]                                      0.64205E-02 
c  Velocity[Y]                                      0.69075E-03 
c  Velocity[Z]                                      0.75800E-03 
c  Pressure     0.84522E-04     770   0.41286E-02   0.18947E+00 0.83065E+01 
c  TempC        0.99048E+04      22   0.59345E-02   0.28594E+04 0.37415E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045332                          1960


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.24252          1.6486         0.98284         0.99821
v  Velocity[Y]            -0.31809         0.40187     -0.00084673     -0.00050872
v  Velocity[Z]            -0.46162         0.20878      -0.0030303      -0.0023886
v  ǁVelocityǁ             0.2471          1.6704         0.98359         0.99853
v  Pressure              -0.029893          2.1268          1.8156           1.817
v  TempC                    14.751          365.34          266.88             271
v  CourantNb                     1           2.206          1.0005          1.0001
v  FourierNb             0.0053975         0.10646        0.021314         0.01654
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082733       0.0023535        0.003069


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2478          1.0218          1.0167


 TIME FOR THE TIME STEP               32:        0.20392E+02

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


 INSTANT    0.330000000E+00   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53257E-01 0.15697E+00
   Friction velocity        uk    :  0.53257E-01 0.15697E+00
   Dimensionless distance   yplus :  0.31475E+01 0.14610E+02
   Friction thermal sca.    tstar :  0.10235E+01 0.77224E+02
   Rough dim-less th. sca.  tplus :  0.23484E+01 0.10901E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34712E-01      19   0.78886E-02   0.75439E-02 0.18829E+01 
c  Velocity[X]                                      0.61514E-02 
c  Velocity[Y]                                      0.65724E-03 
c  Velocity[Z]                                      0.73524E-03 
c  Pressure     0.76354E-04     734   0.35212E-02   0.17111E+00 0.66542E+01 
c  TempC        0.98860E+04      22   0.59206E-02   0.28339E+04 0.37308E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045405                          1955


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.23587          1.6646         0.98248         0.99822
v  Velocity[Y]            -0.31626         0.40204     -0.00084571     -0.00050883
v  Velocity[Z]            -0.46913         0.21137        -0.00312      -0.0024588
v  ǁVelocityǁ            0.24091          1.6817         0.98323         0.99855
v  Pressure              -0.038279          2.1646          1.8469          1.8483
v  TempC                    13.915          366.92          266.11          270.15
v  CourantNb                     1          2.2024          1.0005          1.0001
v  FourierNb             0.0053956         0.10636        0.021326        0.016543
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082731       0.0023544       0.0030688


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2442          1.0218          1.0167


 TIME FOR THE TIME STEP               33:        0.19595E+02

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


 INSTANT    0.340000000E+00   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51490E-01 0.15755E+00
   Friction velocity        uk    :  0.51490E-01 0.15755E+00
   Dimensionless distance   yplus :  0.28410E+01 0.14598E+02
   Friction thermal sca.    tstar :  0.12299E+01 0.77285E+02
   Rough dim-less th. sca.  tplus :  0.21197E+01 0.10891E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34724E-01      19   0.77572E-02   0.76384E-02 0.18907E+01 
c  Velocity[X]                                      0.62267E-02 
c  Velocity[Y]                                      0.68311E-03 
c  Velocity[Z]                                      0.72853E-03 
c  Pressure     0.81736E-04     718   0.38844E-02   0.18365E+00 0.69281E+01 
c  TempC        0.98672E+04      22   0.59141E-02   0.27962E+04 0.37119E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step       0.0004545                          1944


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20954           1.676         0.98211         0.99822
v  Velocity[Y]            -0.32819         0.40454     -0.00084577     -0.00051022
v  Velocity[Z]            -0.47453         0.21259      -0.0032042      -0.0025256
v  ǁVelocityǁ            0.21136          1.7025         0.98287         0.99856
v  Pressure              -0.023743          2.1969          1.8801          1.8815
v  TempC                     9.531           368.1          265.35          269.29
v  CourantNb                     1          2.2002          1.0004          1.0001
v  FourierNb             0.0053938         0.10608        0.021339        0.016546
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082724       0.0023553       0.0030686


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054           2.242          1.0218          1.0167


 TIME FOR THE TIME STEP               34:        0.19530E+02

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


 INSTANT    0.350000000E+00   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50578E-01 0.15825E+00
   Friction velocity        uk    :  0.50578E-01 0.15825E+00
   Dimensionless distance   yplus :  0.25449E+01 0.14624E+02
   Friction thermal sca.    tstar :  0.68665E+00 0.76186E+02
   Rough dim-less th. sca.  tplus :  0.18988E+01 0.10911E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34736E-01      19   0.78827E-02   0.73887E-02 0.18546E+01 
c  Velocity[X]                                      0.60105E-02 
c  Velocity[Y]                                      0.65836E-03 
c  Velocity[Z]                                      0.71980E-03 
c  Pressure     0.75626E-04     729   0.33270E-02   0.16991E+00 0.57518E+01 
c  TempC        0.98484E+04      22   0.59221E-02   0.27628E+04 0.36930E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045431                          1927


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21047          1.6865         0.98174         0.99823
v  Velocity[Y]            -0.33028         0.40742     -0.00084441     -0.00051059
v  Velocity[Z]            -0.48088         0.21204      -0.0032885      -0.0025913
v  ǁVelocityǁ            0.21385          1.7148         0.98251         0.99857
v  Pressure              -0.030853          2.2238          1.9081          1.9095
v  TempC                    2.7896          368.41          264.58          268.44
v  CourantNb                     1          2.2011          1.0004          1.0001
v  FourierNb              0.005392         0.10585        0.021351        0.016549
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082721       0.0023562       0.0030684


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2429          1.0218          1.0167


 TIME FOR THE TIME STEP               35:        0.17710E+02

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


 INSTANT    0.360000000E+00   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49555E-01 0.15892E+00
   Friction velocity        uk    :  0.49555E-01 0.15892E+00
   Dimensionless distance   yplus :  0.31709E+01 0.14637E+02
   Friction thermal sca.    tstar :  0.78092E+00 0.74332E+02
   Rough dim-less th. sca.  tplus :  0.23658E+01 0.10920E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34748E-01      19   0.79479E-02   0.76344E-02 0.18841E+01 
c  Velocity[X]                                      0.62505E-02 
c  Velocity[Y]                                      0.66291E-03 
c  Velocity[Z]                                      0.72093E-03 
c  Pressure     0.80542E-04     734   0.36914E-02   0.18155E+00 0.58588E+01 
c  TempC        0.98295E+04      22   0.60134E-02   0.27373E+04 0.36837E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045574                          1918


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21591          1.6981         0.98138         0.99824
v  Velocity[Y]            -0.33857         0.41106     -0.00084494       -0.000513
v  Velocity[Z]            -0.48396         0.21197      -0.0033708      -0.0026564
v  ǁVelocityǁ            0.21811          1.7269         0.98216         0.99858
v  Pressure              -0.022134          2.2527           1.937          1.9385
v  TempC                  -0.78655           366.1          263.81          267.59
v  CourantNb                     1          2.1943          1.0004          1.0001
v  FourierNb             0.0053903         0.10577        0.021364        0.016552
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082715       0.0023571       0.0030682


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054           2.236          1.0218          1.0167


 TIME FOR THE TIME STEP               36:        0.17760E+02

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


 INSTANT    0.370000000E+00   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55322E-01 0.15959E+00
   Friction velocity        uk    :  0.55322E-01 0.15959E+00
   Dimensionless distance   yplus :  0.29620E+01 0.14652E+02
   Friction thermal sca.    tstar :  0.56052E+00 0.74619E+02
   Rough dim-less th. sca.  tplus :  0.22100E+01 0.10932E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34760E-01      19   0.78737E-02   0.76759E-02 0.18869E+01 
c  Velocity[X]                                      0.62775E-02 
c  Velocity[Y]                                      0.67933E-03 
c  Velocity[Z]                                      0.71901E-03 
c  Pressure     0.76657E-04     732   0.33738E-02   0.17317E+00 0.51603E+01 
c  TempC        0.98106E+04      22   0.58533E-02   0.27159E+04 0.36750E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045713                          1897


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22228          1.7091         0.98102         0.99824
v  Velocity[Y]            -0.31806         0.41249     -0.00084432     -0.00051522
v  Velocity[Z]            -0.48888         0.19838      -0.0034464       -0.002718
v  ǁVelocityǁ            0.22346          1.7303         0.98181         0.99859
v  Pressure              -0.039899          2.2797          1.9628          1.9643
v  TempC                    7.7798          342.08          263.05          266.73
v  CourantNb                     1          2.1875          1.0004          1.0001
v  FourierNb             0.0053885         0.10588        0.021376        0.016555
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082706        0.002358        0.003068


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2293          1.0218          1.0167


 TIME FOR THE TIME STEP               37:        0.17802E+02

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


 INSTANT    0.380000000E+00   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.58243E-01 0.15988E+00
   Friction velocity        uk    :  0.58243E-01 0.15988E+00
   Dimensionless distance   yplus :  0.26358E+01 0.14626E+02
   Friction thermal sca.    tstar :  0.90483E+00 0.74140E+02
   Rough dim-less th. sca.  tplus :  0.19666E+01 0.10913E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34771E-01      19   0.78228E-02   0.77320E-02 0.18882E+01 
c  Velocity[X]                                      0.63246E-02 
c  Velocity[Y]                                      0.67000E-03 
c  Velocity[Z]                                      0.73741E-03 
c  Pressure     0.84919E-04     732   0.40624E-02   0.19223E+00 0.68688E+01 
c  TempC        0.97917E+04      22   0.59236E-02   0.26770E+04 0.36558E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045559                          1878


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.23052          1.7256         0.98066         0.99824
v  Velocity[Y]            -0.32387         0.41472     -0.00084663      -0.0005186
v  Velocity[Z]            -0.49259         0.20391      -0.0035194      -0.0027773
v  ǁVelocityǁ            0.23768          1.7528         0.98145          0.9986
v  Pressure              -0.022368          2.3103          1.9978          1.9993
v  TempC                    5.2267          334.32          262.28          265.88
v  CourantNb               0.99193          2.1949          1.0004          1.0001
v  FourierNb              0.005387         0.10609        0.021388        0.016558
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001         0.00827       0.0023588       0.0030678


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2367          1.0218          1.0167


 TIME FOR THE TIME STEP               38:        0.17784E+02

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


 INSTANT    0.390000000E+00   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60485E-01 0.16075E+00
   Friction velocity        uk    :  0.60485E-01 0.16075E+00
   Dimensionless distance   yplus :  0.31865E+01 0.14625E+02
   Friction thermal sca.    tstar :  0.83261E+00 0.72235E+02
   Rough dim-less th. sca.  tplus :  0.23775E+01 0.10912E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34783E-01      19   0.76878E-02   0.76060E-02 0.18734E+01 
c  Velocity[X]                                      0.62330E-02 
c  Velocity[Y]                                      0.66199E-03 
c  Velocity[Z]                                      0.71102E-03 
c  Pressure     0.76840E-04     715   0.34487E-02   0.17441E+00 0.54074E+01 
c  TempC        0.97727E+04      22   0.58122E-02   0.26476E+04 0.36384E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045285                          1858


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22606          1.7325         0.98031         0.99825
v  Velocity[Y]            -0.33976         0.41375     -0.00084449     -0.00051885
v  Velocity[Z]            -0.50184         0.20616      -0.0035936      -0.0028364
v  ǁVelocityǁ            0.23191          1.7642         0.98111         0.99862
v  Pressure              -0.026367          2.3445          2.0257          2.0273
v  TempC                     12.36          342.68          261.52          265.03
v  CourantNb                     1          2.2082          1.0004          1.0001
v  FourierNb             0.0053853         0.10595        0.021401        0.016561
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082692       0.0023597       0.0030676


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054            2.25          1.0218          1.0167


 TIME FOR THE TIME STEP               39:        0.17481E+02

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


 INSTANT    0.400000000E+00   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57156E-01 0.16104E+00
   Friction velocity        uk    :  0.57156E-01 0.16104E+00
   Dimensionless distance   yplus :  0.29203E+01 0.14626E+02
   Friction thermal sca.    tstar :  0.79576E+00 0.71169E+02
   Rough dim-less th. sca.  tplus :  0.21789E+01 0.10913E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34795E-01      19   0.76721E-02   0.72679E-02 0.18326E+01 
c  Velocity[X]                                      0.59210E-02 
c  Velocity[Y]                                      0.64812E-03 
c  Velocity[Z]                                      0.69873E-03 
c  Pressure     0.78072E-04     734   0.35716E-02   0.17733E+00 0.54878E+01 
c  TempC        0.97538E+04      22   0.59580E-02   0.26250E+04 0.36285E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045351                          1835


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22178           1.747         0.97995         0.99826
v  Velocity[Y]            -0.34799         0.41802       -0.000846     -0.00052191
v  Velocity[Z]            -0.50123         0.20827       -0.003667      -0.0028948
v  ǁVelocityǁ            0.22324          1.7791         0.98076         0.99863
v  Pressure               -0.01294          2.3718          2.0545          2.0561
v  TempC                    10.092          349.91          260.76          264.18
v  CourantNb                     1           2.205          1.0004          1.0001
v  FourierNb             0.0053836         0.10707        0.021413        0.016564
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082684       0.0023606       0.0030674


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2468          1.0219          1.0167


 TIME FOR THE TIME STEP               40:        0.17764E+02

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


 INSTANT    0.410000000E+00   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55076E-01 0.16182E+00
   Friction velocity        uk    :  0.55076E-01 0.16182E+00
   Dimensionless distance   yplus :  0.25902E+01 0.14635E+02
   Friction thermal sca.    tstar :  0.80966E+00 0.70746E+02
   Rough dim-less th. sca.  tplus :  0.19326E+01 0.10919E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34807E-01      19   0.76253E-02   0.72371E-02 0.18245E+01 
c  Velocity[X]                                      0.58915E-02 
c  Velocity[Y]                                      0.64140E-03 
c  Velocity[Z]                                      0.70420E-03 
c  Pressure     0.74078E-04     697   0.31438E-02   0.16839E+00 0.41593E+01 
c  TempC        0.97349E+04      22   0.58869E-02   0.26041E+04 0.36231E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045802                          1824


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.23418          1.7573          0.9796         0.99827
v  Velocity[Y]            -0.36379         0.42238     -0.00084703     -0.00052386
v  Velocity[Z]            -0.51174          0.2076      -0.0037408      -0.0029517
v  ǁVelocityǁ            0.23693          1.7832         0.98042         0.99864
v  Pressure              -0.031542          2.3951          2.0765          2.0781
v  TempC                    17.793          353.87             260          263.33
v  CourantNb                     1          2.1833          1.0004          1.0001
v  FourierNb              0.005382         0.10733        0.021426        0.016567
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082677       0.0023615       0.0030673


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2251          1.0219          1.0167


 TIME FOR THE TIME STEP               41:        0.17307E+02

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


 INSTANT    0.420000000E+00   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50804E-01 0.16227E+00
   Friction velocity        uk    :  0.50804E-01 0.16227E+00
   Dimensionless distance   yplus :  0.30873E+01 0.14660E+02
   Friction thermal sca.    tstar :  0.75670E+00 0.69858E+02
   Rough dim-less th. sca.  tplus :  0.23034E+01 0.10938E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34819E-01      19   0.75993E-02   0.71419E-02 0.18123E+01 
c  Velocity[X]                                      0.58173E-02 
c  Velocity[Y]                                      0.63249E-03 
c  Velocity[Z]                                      0.69207E-03 
c  Pressure     0.80387E-04     735   0.37209E-02   0.18311E+00 0.54982E+01 
c  TempC        0.97158E+04      22   0.59428E-02   0.25672E+04 0.36048E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045802                          1813


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21603          1.7679         0.97925         0.99827
v  Velocity[Y]            -0.35939         0.42674     -0.00084742     -0.00052715
v  Velocity[Z]            -0.51377         0.19632      -0.0038078      -0.0030055
v  ǁVelocityǁ            0.21838          1.7998         0.98008         0.99865
v  Pressure              -0.018658          2.4243           2.106          2.1076
v  TempC                    14.621          356.98          259.24          262.48
v  CourantNb                     1          2.1833          1.0004          1.0001
v  FourierNb             0.0053803          0.1075        0.021438         0.01657
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082671       0.0023624       0.0030671


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2251          1.0219          1.0167


 TIME FOR THE TIME STEP               42:        0.17816E+02

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


 INSTANT    0.430000000E+00   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447994E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48935E-01 0.16306E+00
   Friction velocity        uk    :  0.48935E-01 0.16306E+00
   Dimensionless distance   yplus :  0.27615E+01 0.14632E+02
   Friction thermal sca.    tstar :  0.70759E+00 0.70585E+02
   Rough dim-less th. sca.  tplus :  0.20604E+01 0.10917E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34831E-01      19   0.76926E-02   0.69606E-02 0.17869E+01 
c  Velocity[X]                                      0.56640E-02 
c  Velocity[Y]                                      0.62751E-03 
c  Velocity[Z]                                      0.66908E-03 
c  Pressure     0.73873E-04     703   0.33058E-02   0.16848E+00 0.46793E+01 
c  TempC        0.96968E+04      22   0.58307E-02   0.25585E+04 0.36078E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step        0.000456                          1801


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20175          1.7782         0.97891         0.99828
v  Velocity[Y]             -0.3667          0.4281     -0.00084891     -0.00053097
v  Velocity[Z]            -0.52042         0.20022      -0.0038785        -0.00306
v  ǁVelocityǁ            0.20414          1.8108         0.97974         0.99866
v  Pressure              -0.021129          2.4484          2.1315          2.1331
v  TempC                    9.8917           357.5          258.48          261.64
v  CourantNb                     1           2.193          1.0004          1.0001
v  FourierNb             0.0053786         0.10748         0.02145        0.016573
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082667       0.0023633       0.0030669


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2348          1.0219          1.0167


 TIME FOR THE TIME STEP               43:        0.17157E+02

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


 INSTANT    0.440000000E+00   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447994E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52523E-01 0.16323E+00
   Friction velocity        uk    :  0.52523E-01 0.16323E+00
   Dimensionless distance   yplus :  0.32203E+01 0.14627E+02
   Friction thermal sca.    tstar :  0.10718E+01 0.69743E+02
   Rough dim-less th. sca.  tplus :  0.24027E+01 0.10913E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34842E-01      19   0.76318E-02   0.74782E-02 0.18459E+01 
c  Velocity[X]                                      0.61532E-02 
c  Velocity[Y]                                      0.64172E-03 
c  Velocity[Z]                                      0.68329E-03 
c  Pressure     0.79008E-04     713   0.35429E-02   0.18079E+00 0.45342E+01 
c  TempC        0.96777E+04      22   0.59990E-02   0.25223E+04 0.35877E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045721                          1794


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.24237           1.792         0.97856         0.99828
v  Velocity[Y]            -0.36418         0.43097     -0.00085168     -0.00053511
v  Velocity[Z]            -0.51662         0.20251      -0.0039441      -0.0031128
v  ǁVelocityǁ             0.2468           1.824          0.9794         0.99867
v  Pressure              -0.010944          2.4734          2.1564           2.158
v  TempC                    6.8762          359.04          257.72          260.79
v  CourantNb                     1          2.1872          1.0004          1.0001
v  FourierNb              0.005377         0.10694        0.021463        0.016576
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082662       0.0023642       0.0030668


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2289          1.0219          1.0167


 TIME FOR THE TIME STEP               44:        0.17536E+02

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


 INSTANT    0.450000000E+00   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55673E-01 0.16387E+00
   Friction velocity        uk    :  0.55673E-01 0.16387E+00
   Dimensionless distance   yplus :  0.29993E+01 0.14628E+02
   Friction thermal sca.    tstar :  0.10376E+01 0.70900E+02
   Rough dim-less th. sca.  tplus :  0.22378E+01 0.10914E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34854E-01      19   0.74768E-02   0.72892E-02 0.18182E+01 
c  Velocity[X]                                      0.59678E-02 
c  Velocity[Y]                                      0.63768E-03 
c  Velocity[Z]                                      0.68368E-03 
c  Pressure     0.74677E-04     702   0.31422E-02   0.17113E+00 0.38258E+01 
c  TempC        0.96586E+04      22   0.59730E-02   0.25138E+04 0.35894E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046128                          1779


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22325          1.7955         0.97822         0.99829
v  Velocity[Y]            -0.36114         0.42889     -0.00085362     -0.00053851
v  Velocity[Z]            -0.52324         0.20316      -0.0040048      -0.0031616
v  ǁVelocityǁ            0.22464          1.8292         0.97907         0.99868
v  Pressure              -0.021361          2.4945          2.1776          2.1793
v  TempC                    6.3933          358.85          256.97          259.94
v  CourantNb               0.97649          2.1679          1.0004          1.0001
v  FourierNb             0.0053754         0.10652        0.021475        0.016579
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082657       0.0023651       0.0030666


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2096          1.0219          1.0167


 TIME FOR THE TIME STEP               45:        0.17130E+02

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


 INSTANT    0.460000000E+00   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54519E-01 0.16393E+00
   Friction velocity        uk    :  0.54519E-01 0.16393E+00
   Dimensionless distance   yplus :  0.26380E+01 0.14647E+02
   Friction thermal sca.    tstar :  0.98135E+00 0.71327E+02
   Rough dim-less th. sca.  tplus :  0.19682E+01 0.10928E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34865E-01      19   0.75072E-02   0.69340E-02 0.17782E+01 
c  Velocity[X]                                      0.56563E-02 
c  Velocity[Y]                                      0.61886E-03 
c  Velocity[Z]                                      0.65878E-03 
c  Pressure     0.77307E-04     715   0.35496E-02   0.17750E+00 0.46509E+01 
c  TempC        0.96394E+04      22   0.59030E-02   0.24831E+04 0.35756E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046137                          1772


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              0.2338          1.8091         0.97788         0.99829
v  Velocity[Y]            -0.36531         0.42655      -0.0008541     -0.00054188
v  Velocity[Z]            -0.52234         0.20527      -0.0040685       -0.003212
v  ǁVelocityǁ             0.2397          1.8428         0.97873          0.9987
v  Pressure              -0.008638          2.5217          2.2037          2.2054
v  TempC                    6.4512          334.13          256.21           259.1
v  CourantNb                     1          2.1675          1.0004          1.0001
v  FourierNb              0.005374         0.10616        0.021488        0.016582
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082653       0.0023659       0.0030664


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2093          1.0219          1.0167


 TIME FOR THE TIME STEP               46:        0.17710E+02

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


 INSTANT    0.470000000E+00   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53022E-01 0.16465E+00
   Friction velocity        uk    :  0.53022E-01 0.16465E+00
   Dimensionless distance   yplus :  0.30990E+01 0.14669E+02
   Friction thermal sca.    tstar :  0.91919E+00 0.71047E+02
   Rough dim-less th. sca.  tplus :  0.23122E+01 0.10945E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34877E-01      19   0.74964E-02   0.71115E-02 0.17972E+01 
c  Velocity[X]                                      0.58151E-02 
c  Velocity[Y]                                      0.62167E-03 
c  Velocity[Z]                                      0.67473E-03 
c  Pressure     0.73797E-04     700   0.31445E-02   0.16978E+00 0.35906E+01 
c  TempC        0.96202E+04      22   0.57890E-02   0.24479E+04 0.35558E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00045961                          1743


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22703          1.8161         0.97754          0.9983
v  Velocity[Y]            -0.36115         0.42817     -0.00085697     -0.00054536
v  Velocity[Z]             -0.5243         0.19516       -0.004127      -0.0032593
v  ǁVelocityǁ            0.23116          1.8476         0.97841         0.99871
v  Pressure              -0.023929          2.5415           2.224          2.2257
v  TempC                    8.0763          326.99          255.46          258.25
v  CourantNb                     1          2.1758          1.0004          1.0001
v  FourierNb             0.0053725         0.10588          0.0215        0.016585
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082648       0.0023668       0.0030663


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2175          1.0219          1.0167


 TIME FOR THE TIME STEP               47:        0.17496E+02

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


 INSTANT    0.480000000E+00   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52614E-01 0.16507E+00
   Friction velocity        uk    :  0.52614E-01 0.16507E+00
   Dimensionless distance   yplus :  0.27631E+01 0.14656E+02
   Friction thermal sca.    tstar :  0.85633E+00 0.71500E+02
   Rough dim-less th. sca.  tplus :  0.20616E+01 0.10935E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34888E-01      19   0.73550E-02   0.70511E-02 0.17874E+01 
c  Velocity[X]                                      0.57504E-02 
c  Velocity[Y]                                      0.62848E-03 
c  Velocity[Z]                                      0.67219E-03 
c  Pressure     0.79298E-04     717   0.36393E-02   0.18266E+00 0.48576E+01 
c  TempC        0.96009E+04      22   0.59951E-02   0.24191E+04 0.35392E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046243                          1725


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20075          1.8278          0.9772          0.9983
v  Velocity[Y]            -0.37197         0.43177     -0.00085864      -0.0005499
v  Velocity[Z]             -0.5244          0.1976      -0.0041863      -0.0033064
v  ǁVelocityǁ            0.20133          1.8618         0.97807         0.99872
v  Pressure              -0.012249          2.5694           2.252          2.2537
v  TempC                    9.7411          332.69          254.71          257.41
v  CourantNb                     1          2.1625          1.0004          1.0001
v  FourierNb             0.0053711         0.10677        0.021512        0.016588
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082646       0.0023677       0.0030661


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2043          1.0219          1.0167


 TIME FOR THE TIME STEP               48:        0.17780E+02

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


 INSTANT    0.490000000E+00   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50435E-01 0.16568E+00
   Friction velocity        uk    :  0.50435E-01 0.16568E+00
   Dimensionless distance   yplus :  0.24717E+01 0.14655E+02
   Friction thermal sca.    tstar :  0.79583E+00 0.70553E+02
   Rough dim-less th. sca.  tplus :  0.18442E+01 0.10934E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34900E-01      19   0.73526E-02   0.66487E-02 0.17326E+01 
c  Velocity[X]                                      0.54061E-02 
c  Velocity[Y]                                      0.59700E-03 
c  Velocity[Z]                                      0.64555E-03 
c  Pressure     0.72446E-04     703   0.31306E-02   0.16688E+00 0.40596E+01 
c  TempC        0.95815E+04      22   0.60512E-02   0.24235E+04 0.35534E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046513                          1711


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21771          1.8352         0.97687         0.99831
v  Velocity[Y]            -0.37383         0.43319     -0.00085953     -0.00055414
v  Velocity[Z]            -0.53137         0.20013      -0.0042443      -0.0033521
v  ǁVelocityǁ            0.21792          1.8701         0.97775         0.99873
v  Pressure              -0.017328          2.5913          2.2755          2.2773
v  TempC                    12.626          338.45          253.96          256.57
v  CourantNb                     1          2.1499          1.0004          1.0001
v  FourierNb             0.0053697          0.1072        0.021525        0.016591
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082642       0.0023686        0.003066


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1917           1.022          1.0167


 TIME FOR THE TIME STEP               49:        0.20890E+02

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


 INSTANT    0.500000000E+00   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447994E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49664E-01 0.16589E+00
   Friction velocity        uk    :  0.49664E-01 0.16589E+00
   Dimensionless distance   yplus :  0.31081E+01 0.14652E+02
   Friction thermal sca.    tstar :  0.73977E+00 0.68661E+02
   Rough dim-less th. sca.  tplus :  0.23190E+01 0.10932E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         50, Physical time    0.50000E+00


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
 End writing


 Time for restart files:    0.14700E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34912E-01      19   0.74420E-02   0.68337E-02 0.17559E+01 
c  Velocity[X]                                      0.55829E-02 
c  Velocity[Y]                                      0.60276E-03 
c  Velocity[Z]                                      0.64807E-03 
c  Pressure     0.76493E-04     718   0.34572E-02   0.17665E+00 0.42099E+01 
c  TempC        0.95622E+04      21   0.58925E-02   0.24014E+04 0.35384E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046181                          1700


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21117          1.8467         0.97653         0.99831
v  Velocity[Y]            -0.37033          0.4342     -0.00086358      -0.0005594
v  Velocity[Z]              -0.527         0.20083      -0.0042979      -0.0033953
v  ǁVelocityǁ            0.21202          1.8818         0.97742         0.99874
v  Pressure             -0.0047682          2.6154          2.3002           2.302
v  TempC                    8.9385          341.97          253.21          255.72
v  CourantNb               0.99963          2.1654          1.0004          1.0001
v  FourierNb             0.0053684         0.10751        0.021537        0.016594
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082639       0.0023695       0.0030658


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.2072           1.022          1.0167


 TIME FOR THE TIME STEP               50:        0.20329E+02

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


 INSTANT    0.510000000E+00   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54624E-01 0.16662E+00
   Friction velocity        uk    :  0.54624E-01 0.16662E+00
   Dimensionless distance   yplus :  0.28668E+01 0.14669E+02
   Friction thermal sca.    tstar :  0.68845E+00 0.68233E+02
   Rough dim-less th. sca.  tplus :  0.21390E+01 0.10945E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34923E-01      19   0.74791E-02   0.70645E-02 0.17835E+01 
c  Velocity[X]                                      0.57936E-02 
c  Velocity[Y]                                      0.61955E-03 
c  Velocity[Z]                                      0.65142E-03 
c  Pressure     0.73961E-04     698   0.31015E-02   0.17123E+00 0.32862E+01 
c  TempC        0.95428E+04      21   0.59601E-02   0.23651E+04 0.35147E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046483                          1685


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21817          1.8505         0.97621         0.99832
v  Velocity[Y]            -0.37524         0.43458     -0.00086656     -0.00056362
v  Velocity[Z]            -0.53504         0.20105      -0.0043518      -0.0034378
v  ǁVelocityǁ            0.21874          1.8856          0.9771         0.99875
v  Pressure              -0.016281          2.6402          2.3196          2.3214
v  TempC                    7.5164          345.41          252.46          254.88
v  CourantNb                     1          2.1513          1.0004          1.0001
v  FourierNb             0.0053671          0.1079        0.021549        0.016597
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082634       0.0023704       0.0030657


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1931           1.022          1.0167


 TIME FOR THE TIME STEP               51:        0.19416E+02

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


 INSTANT    0.520000000E+00   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.56491E-01 0.16683E+00
   Friction velocity        uk    :  0.56491E-01 0.16683E+00
   Dimensionless distance   yplus :  0.25684E+01 0.14687E+02
   Friction thermal sca.    tstar :  0.90098E+00 0.67557E+02
   Rough dim-less th. sca.  tplus :  0.19163E+01 0.10958E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34934E-01      19   0.73859E-02   0.69922E-02 0.17760E+01 
c  Velocity[X]                                      0.57148E-02 
c  Velocity[Y]                                      0.61525E-03 
c  Velocity[Z]                                      0.66221E-03 
c  Pressure     0.77468E-04     720   0.34420E-02   0.17971E+00 0.39389E+01 
c  TempC        0.95232E+04      21   0.60945E-02   0.23543E+04 0.35193E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046622                          1669


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.24205           1.862         0.97587         0.99832
v  Velocity[Y]              -0.363         0.43867     -0.00086832     -0.00056792
v  Velocity[Z]            -0.53827         0.19418      -0.0044063        -0.00348
v  ǁVelocityǁ            0.24923          1.8981         0.97678         0.99876
v  Pressure             -0.0053957          2.6601          2.3432           2.345
v  TempC                    3.0582          346.24          251.72          254.04
v  CourantNb                0.9935          2.1449          1.0004          1.0001
v  FourierNb             0.0053658         0.10709        0.021561        0.016601
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082635       0.0023713       0.0030655


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1867           1.022          1.0167


 TIME FOR THE TIME STEP               52:        0.20072E+02

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


 INSTANT    0.530000000E+00   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55581E-01 0.16717E+00
   Friction velocity        uk    :  0.55581E-01 0.16717E+00
   Dimensionless distance   yplus :  0.30787E+01 0.14660E+02
   Friction thermal sca.    tstar :  0.10230E+01 0.67733E+02
   Rough dim-less th. sca.  tplus :  0.22971E+01 0.10938E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34946E-01      19   0.72977E-02   0.67283E-02 0.17444E+01 
c  Velocity[X]                                      0.54942E-02 
c  Velocity[Y]                                      0.59349E-03 
c  Velocity[Z]                                      0.64066E-03 
c  Pressure     0.71882E-04     698   0.31129E-02   0.16696E+00 0.33770E+01 
c  TempC        0.95037E+04      21   0.58913E-02   0.23433E+04 0.35152E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046658                          1660


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.23604          1.8718         0.97555         0.99833
v  Velocity[Y]            -0.37627         0.44007     -0.00087008     -0.00057406
v  Velocity[Z]            -0.54662         0.19306      -0.0044619      -0.0035214
v  ǁVelocityǁ            0.23669           1.906         0.97646         0.99877
v  Pressure              -0.012183          2.6795          2.3635          2.3653
v  TempC                 0.0046201          348.07          250.97           253.2
v  CourantNb                     1          2.1432          1.0004          1.0001
v  FourierNb             0.0053646         0.10683        0.021574        0.016604
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082633       0.0023722       0.0030654


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054           2.185           1.022          1.0167


 TIME FOR THE TIME STEP               53:        0.19735E+02

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


 INSTANT    0.540000000E+00   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55225E-01 0.16772E+00
   Friction velocity        uk    :  0.55225E-01 0.16772E+00
   Dimensionless distance   yplus :  0.27433E+01 0.14649E+02
   Friction thermal sca.    tstar :  0.96595E+00 0.68031E+02
   Rough dim-less th. sca.  tplus :  0.20468E+01 0.10930E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34957E-01      19   0.72957E-02   0.66782E-02 0.17299E+01 
c  Velocity[X]                                      0.54469E-02 
c  Velocity[Y]                                      0.59079E-03 
c  Velocity[Z]                                      0.64056E-03 
c  Pressure     0.74806E-04     699   0.32777E-02   0.17413E+00 0.35255E+01 
c  TempC        0.94841E+04      21   0.58930E-02   0.23002E+04 0.34889E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046827                          1643


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20802          1.8805         0.97522         0.99833
v  Velocity[Y]            -0.37795         0.44257     -0.00087244     -0.00057871
v  Velocity[Z]            -0.54711         0.19546      -0.0045137      -0.0035617
v  ǁVelocityǁ            0.20946          1.9166         0.97614         0.99878
v  Pressure               0.003749           2.705          2.3849          2.3868
v  TempC                   -1.6989           348.1          250.23          252.35
v  CourantNb                     1          2.1355          1.0004          1.0001
v  FourierNb             0.0053634         0.10685        0.021586        0.016607
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082629       0.0023731       0.0030653


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1773           1.022          1.0167


 TIME FOR THE TIME STEP               54:        0.18964E+02

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


 INSTANT    0.550000000E+00   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55103E-01 0.16807E+00
   Friction velocity        uk    :  0.55103E-01 0.16807E+00
   Dimensionless distance   yplus :  0.25478E+01 0.14645E+02
   Friction thermal sca.    tstar :  0.90436E+00 0.67883E+02
   Rough dim-less th. sca.  tplus :  0.19009E+01 0.10927E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34969E-01      19   0.72253E-02   0.67225E-02 0.17357E+01 
c  Velocity[X]                                      0.54938E-02 
c  Velocity[Y]                                      0.59769E-03 
c  Velocity[Z]                                      0.63097E-03 
c  Pressure     0.71395E-04     632   0.29176E-02   0.16633E+00 0.23856E+01 
c  TempC        0.94645E+04      21   0.57589E-02   0.22834E+04 0.34798E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00047027                          1629


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.23984          1.8863          0.9749         0.99834
v  Velocity[Y]            -0.38277         0.44558     -0.00087628     -0.00058483
v  Velocity[Z]            -0.55591         0.19521      -0.0045604      -0.0035989
v  ǁVelocityǁ            0.24276          1.9207         0.97583         0.99879
v  Pressure             -0.0077804          2.7197          2.3994          2.4013
v  TempC                    16.178          324.84          249.49          251.51
v  CourantNb                     1          2.1264          1.0004          1.0001
v  FourierNb             0.0053623         0.10655        0.021599         0.01661
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082621        0.002374       0.0030651


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1682           1.022          1.0167


 TIME FOR THE TIME STEP               55:        0.17865E+02

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


 INSTANT    0.560000000E+00   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54008E-01 0.16843E+00
   Friction velocity        uk    :  0.54008E-01 0.16843E+00
   Dimensionless distance   yplus :  0.31272E+01 0.14640E+02
   Friction thermal sca.    tstar :  0.84190E+00 0.67737E+02
   Rough dim-less th. sca.  tplus :  0.23333E+01 0.10923E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34980E-01      19   0.72536E-02   0.65613E-02 0.17123E+01 
c  Velocity[X]                                      0.53397E-02 
c  Velocity[Y]                                      0.59714E-03 
c  Velocity[Z]                                      0.62442E-03 
c  Pressure     0.74083E-04     700   0.31983E-02   0.17288E+00 0.29718E+01 
c  TempC        0.94449E+04      21   0.60137E-02   0.22585E+04 0.34718E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046929                          1617


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22262          1.8898         0.97458         0.99834
v  Velocity[Y]            -0.38567         0.44885     -0.00088015     -0.00059073
v  Velocity[Z]            -0.55861         0.19203       -0.004607      -0.0036357
v  ǁVelocityǁ            0.22549          1.9257         0.97551          0.9988
v  Pressure              -0.005172          2.7346          2.4177          2.4196
v  TempC                    16.275          317.48          248.75          250.67
v  CourantNb               0.98022          2.1309          1.0004          1.0001
v  FourierNb             0.0053613          0.1074        0.021611        0.016613
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082617       0.0023748        0.003065


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1726           1.022          1.0167


 TIME FOR THE TIME STEP               56:        0.19665E+02

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


 INSTANT    0.570000000E+00   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447994E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.56286E-01 0.16881E+00
   Friction velocity        uk    :  0.56286E-01 0.16881E+00
   Dimensionless distance   yplus :  0.29197E+01 0.14656E+02
   Friction thermal sca.    tstar :  0.76432E+00 0.68172E+02
   Rough dim-less th. sca.  tplus :  0.21784E+01 0.10935E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34991E-01      19   0.72349E-02   0.66424E-02 0.17221E+01 
c  Velocity[X]                                      0.54139E-02 
c  Velocity[Y]                                      0.58768E-03 
c  Velocity[Z]                                      0.64075E-03 
c  Pressure     0.72765E-04     681   0.30559E-02   0.17004E+00 0.28932E+01 
c  TempC        0.94252E+04      21   0.62723E-02   0.22561E+04 0.34732E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00047255                          1596


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               0.207          1.9024         0.97426         0.99834
v  Velocity[Y]            -0.39386         0.44664     -0.00088139     -0.00059578
v  Velocity[Z]            -0.55762         0.19061      -0.0046493      -0.0036704
v  ǁVelocityǁ              0.209          1.9368          0.9752         0.99881
v  Pressure             -0.0097085          2.7562          2.4356          2.4375
v  TempC                    9.7722          323.08          248.01          249.83
v  CourantNb                     1          2.1162          1.0004          1.0001
v  FourierNb             0.0053602         0.10811        0.021623        0.016616
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082615       0.0023757       0.0030649


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1579           1.022          1.0167


 TIME FOR THE TIME STEP               57:        0.20417E+02

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


 INSTANT    0.580000000E+00   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53493E-01 0.16912E+00
   Friction velocity        uk    :  0.53493E-01 0.16912E+00
   Dimensionless distance   yplus :  0.26780E+01 0.14636E+02
   Friction thermal sca.    tstar :  0.72738E+00 0.68585E+02
   Rough dim-less th. sca.  tplus :  0.19981E+01 0.10920E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35002E-01      19   0.72211E-02   0.64976E-02 0.17040E+01 
c  Velocity[X]                                      0.52891E-02 
c  Velocity[Y]                                      0.58852E-03 
c  Velocity[Z]                                      0.61999E-03 
c  Pressure     0.73935E-04     682   0.32600E-02   0.17324E+00 0.32873E+01 
c  TempC        0.94054E+04      21   0.61922E-02   0.22402E+04 0.34690E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00046894                          1589


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20293          1.9111         0.97394         0.99835
v  Velocity[Y]            -0.39464         0.44619     -0.00088754     -0.00060444
v  Velocity[Z]            -0.55731          0.1915      -0.0046943       -0.003705
v  ǁVelocityǁ            0.20485          1.9478         0.97489         0.99882
v  Pressure              0.0061427          2.7737          2.4562          2.4581
v  TempC                    7.3254          330.54          247.27          248.99
v  CourantNb                     1          2.1325          1.0004          1.0001
v  FourierNb             0.0053594         0.10878        0.021636         0.01662
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001        0.008261       0.0023766       0.0030648


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1743          1.0221          1.0168


 TIME FOR THE TIME STEP               58:        0.18199E+02

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


 INSTANT    0.590000000E+00   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53748E-01 0.16917E+00
   Friction velocity        uk    :  0.53748E-01 0.16917E+00
   Dimensionless distance   yplus :  0.30381E+01 0.14618E+02
   Friction thermal sca.    tstar :  0.67612E+00 0.68047E+02
   Rough dim-less th. sca.  tplus :  0.22668E+01 0.10907E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35014E-01      19   0.72060E-02   0.66354E-02 0.17193E+01 
c  Velocity[X]                                      0.54207E-02 
c  Velocity[Y]                                      0.58516E-03 
c  Velocity[Z]                                      0.62951E-03 
c  Pressure     0.71431E-04     667   0.28356E-02   0.16761E+00 0.21451E+01 
c  TempC        0.93856E+04      21   0.61381E-02   0.22087E+04 0.34480E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00047082                          1585


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.23118          1.9135         0.97363         0.99835
v  Velocity[Y]            -0.39385         0.44223     -0.00089364     -0.00061087
v  Velocity[Z]            -0.56193         0.19173      -0.0047344      -0.0037372
v  ǁVelocityǁ            0.23187           1.948         0.97458         0.99883
v  Pressure              -0.011826          2.7874          2.4696          2.4715
v  TempC                    2.7259          333.89          246.54          248.15
v  CourantNb                     1          2.1239          1.0004          1.0001
v  FourierNb             0.0053585         0.10942        0.021648        0.016623
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082608       0.0023775       0.0030646


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1657          1.0221          1.0168


 TIME FOR THE TIME STEP               59:        0.17733E+02

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


 INSTANT    0.600000000E+00   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.56403E-01 0.16956E+00
   Friction velocity        uk    :  0.56403E-01 0.16956E+00
   Dimensionless distance   yplus :  0.28448E+01 0.14639E+02
   Friction thermal sca.    tstar :  0.10467E+01 0.68255E+02
   Rough dim-less th. sca.  tplus :  0.21226E+01 0.10922E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35024E-01      19   0.71807E-02   0.66225E-02 0.17111E+01 
c  Velocity[X]                                      0.54082E-02 
c  Velocity[Y]                                      0.58200E-03 
c  Velocity[Z]                                      0.63228E-03 
c  Pressure     0.75847E-04     717   0.33161E-02   0.17840E+00 0.31826E+01 
c  TempC        0.93658E+04      21   0.62109E-02   0.22012E+04 0.34512E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00047353                          1567


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20912          1.9257         0.97331         0.99836
v  Velocity[Y]            -0.39611         0.44595     -0.00089507     -0.00061611
v  Velocity[Z]            -0.55878         0.19133      -0.0047726      -0.0037684
v  ǁVelocityǁ            0.21088          1.9624         0.97427         0.99883
v  Pressure              0.0062357          2.8086          2.4898          2.4917
v  TempC                    1.5774          337.42           245.8          247.32
v  CourantNb               0.97873          2.1118          1.0004          1.0001
v  FourierNb             0.0053575         0.10934         0.02166        0.016626
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082606       0.0023784       0.0030645


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1536          1.0221          1.0168


 TIME FOR THE TIME STEP               60:        0.18806E+02

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


 INSTANT    0.610000000E+00   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.56552E-01 0.16979E+00
   Friction velocity        uk    :  0.56552E-01 0.16979E+00
   Dimensionless distance   yplus :  0.25593E+01 0.14639E+02
   Friction thermal sca.    tstar :  0.10368E+01 0.66264E+02
   Rough dim-less th. sca.  tplus :  0.19095E+01 0.10922E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35036E-01      19   0.71256E-02   0.64639E-02 0.16926E+01 
c  Velocity[X]                                      0.52856E-02 
c  Velocity[Y]                                      0.56588E-03 
c  Velocity[Z]                                      0.61243E-03 
c  Pressure     0.70444E-04     660   0.29410E-02   0.16606E+00 0.22079E+01 
c  TempC        0.93459E+04      21   0.62011E-02   0.21661E+04 0.34277E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00047623                          1562


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22639           1.932           0.973         0.99836
v  Velocity[Y]            -0.39496         0.44657      -0.0008968     -0.00062134
v  Velocity[Z]            -0.56421          0.1889      -0.0048142      -0.0037998
v  ǁVelocityǁ             0.2301          1.9687         0.97397         0.99884
v  Pressure            -0.00026967          2.8202          2.5038          2.5057
v  TempC                    10.194          338.83          245.07          246.48
v  CourantNb                     1          2.0998          1.0004          1.0001
v  FourierNb             0.0053567         0.10888        0.021672        0.016629
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082604       0.0023793       0.0030644


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1416          1.0221          1.0168


 TIME FOR THE TIME STEP               61:        0.18363E+02

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


 INSTANT    0.620000000E+00   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57179E-01 0.16994E+00
   Friction velocity        uk    :  0.57179E-01 0.16994E+00
   Dimensionless distance   yplus :  0.31475E+01 0.14658E+02
   Friction thermal sca.    tstar :  0.99904E+00 0.64587E+02
   Rough dim-less th. sca.  tplus :  0.23484E+01 0.10937E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35047E-01      19   0.70323E-02   0.64651E-02 0.16937E+01 
c  Velocity[X]                                      0.52827E-02 
c  Velocity[Y]                                      0.57441E-03 
c  Velocity[Z]                                      0.60804E-03 
c  Pressure     0.72855E-04     681   0.30709E-02   0.17208E+00 0.23823E+01 
c  TempC        0.93259E+04      21   0.60331E-02   0.21511E+04 0.34236E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step       0.0004727                          1551


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.23458          1.9338         0.97269         0.99837
v  Velocity[Y]            -0.39927         0.44571     -0.00089937     -0.00062744
v  Velocity[Z]            -0.56507         0.18914      -0.0048535      -0.0038302
v  ǁVelocityǁ            0.23759            1.97         0.97366         0.99885
v  Pressure               0.002375          2.8381           2.519           2.521
v  TempC                    9.8542          340.56          244.34          245.64
v  CourantNb                     1          2.1155          1.0004          1.0001
v  FourierNb             0.0053559         0.10853        0.021685        0.016632
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082604       0.0023802       0.0030643


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1573          1.0221          1.0168


 TIME FOR THE TIME STEP               62:        0.19639E+02

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


 INSTANT    0.630000000E+00   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.56133E-01 0.17045E+00
   Friction velocity        uk    :  0.56133E-01 0.17045E+00
   Dimensionless distance   yplus :  0.29361E+01 0.14617E+02
   Friction thermal sca.    tstar :  0.95155E+00 0.64609E+02
   Rough dim-less th. sca.  tplus :  0.21907E+01 0.10906E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35058E-01      19   0.70198E-02   0.63360E-02 0.16744E+01 
c  Velocity[X]                                      0.51782E-02 
c  Velocity[Y]                                      0.56948E-03 
c  Velocity[Z]                                      0.58835E-03 
c  Pressure     0.70736E-04     677   0.28693E-02   0.16704E+00 0.22318E+01 
c  TempC        0.93060E+04      21   0.62748E-02   0.21284E+04 0.34094E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00047452                          1548


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.22396          1.9339         0.97238         0.99837
v  Velocity[Y]            -0.40198         0.44894     -0.00090267     -0.00063351
v  Velocity[Z]            -0.57152         0.18789      -0.0048942      -0.0038605
v  ǁVelocityǁ            0.22472          1.9685         0.97336         0.99886
v  Pressure               -0.01732          2.8514          2.5334          2.5353
v  TempC                    9.2221          339.49          243.61           244.8
v  CourantNb                 0.997          2.1074          1.0004          1.0001
v  FourierNb             0.0053551         0.10953        0.021697        0.016636
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082604        0.002381       0.0030642


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1492          1.0221          1.0168


 TIME FOR THE TIME STEP               63:        0.18545E+02

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


 INSTANT    0.640000000E+00   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55122E-01 0.17080E+00
   Friction velocity        uk    :  0.55122E-01 0.17080E+00
   Dimensionless distance   yplus :  0.26507E+01 0.14719E+02
   Friction thermal sca.    tstar :  0.89977E+00 0.64453E+02
   Rough dim-less th. sca.  tplus :  0.19777E+01 0.10982E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35068E-01      19   0.69717E-02   0.61478E-02 0.16475E+01 
c  Velocity[X]                                      0.49893E-02 
c  Velocity[Y]                                      0.56029E-03 
c  Velocity[Z]                                      0.59828E-03 
c  Pressure     0.75983E-04     715   0.35324E-02   0.17967E+00 0.36482E+01 
c  TempC        0.92860E+04      21   0.63779E-02   0.21366E+04 0.34310E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00047775                          1539


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21204          1.9496         0.97207         0.99837
v  Velocity[Y]            -0.40691         0.45183     -0.00090749     -0.00064088
v  Velocity[Z]            -0.56775         0.18869      -0.0049327      -0.0038898
v  ǁVelocityǁ            0.21447          1.9867         0.97306         0.99887
v  Pressure              0.0076212          2.8736          2.5572          2.5592
v  TempC                    9.4221          317.46          242.88          243.97
v  CourantNb                     1          2.0932          1.0004          1.0001
v  FourierNb             0.0053545         0.10991        0.021709        0.016639
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082603       0.0023819       0.0030641


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054           2.135          1.0221          1.0168


 TIME FOR THE TIME STEP               64:        0.19794E+02

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


 INSTANT    0.650000000E+00   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54750E-01 0.17095E+00
   Friction velocity        uk    :  0.54750E-01 0.17095E+00
   Dimensionless distance   yplus :  0.31072E+01 0.14608E+02
   Friction thermal sca.    tstar :  0.84661E+00 0.64792E+02
   Rough dim-less th. sca.  tplus :  0.23183E+01 0.10899E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35080E-01      19   0.69909E-02   0.61436E-02 0.16484E+01 
c  Velocity[X]                                      0.49856E-02 
c  Velocity[Y]                                      0.55765E-03 
c  Velocity[Z]                                      0.60033E-03 
c  Pressure     0.68926E-04     666   0.28741E-02   0.16312E+00 0.25026E+01 
c  TempC        0.92660E+04      21   0.62379E-02   0.21140E+04 0.34159E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048011                          1532


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.19756          1.9586         0.97177         0.99838
v  Velocity[Y]            -0.39658         0.45123     -0.00091175     -0.00064857
v  Velocity[Z]            -0.57103           0.187      -0.0049691      -0.0039169
v  ǁVelocityǁ            0.20046          1.9941         0.97276         0.99888
v  Pressure              0.0023757          2.8936          2.5736          2.5756
v  TempC                    10.166          316.95          242.15          243.13
v  CourantNb                     1          2.0829          1.0004          1.0001
v  FourierNb             0.0053539         0.10994        0.021721        0.016642
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082597       0.0023828        0.003064


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1247          1.0221          1.0168


 TIME FOR THE TIME STEP               65:        0.22533E+02

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


 INSTANT    0.660000000E+00   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53120E-01 0.17134E+00
   Friction velocity        uk    :  0.53120E-01 0.17134E+00
   Dimensionless distance   yplus :  0.28216E+01 0.14758E+02
   Friction thermal sca.    tstar :  0.79473E+00 0.65630E+02
   Rough dim-less th. sca.  tplus :  0.21052E+01 0.11011E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35091E-01      19   0.70054E-02   0.62504E-02 0.16576E+01 
c  Velocity[X]                                      0.51103E-02 
c  Velocity[Y]                                      0.55747E-03 
c  Velocity[Z]                                      0.58265E-03 
c  Pressure     0.71364E-04     680   0.29785E-02   0.16930E+00 0.21612E+01 
c  TempC        0.92459E+04      21   0.63773E-02   0.20784E+04 0.33890E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00047757                          1529


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20233          1.9626         0.97146         0.99838
v  Velocity[Y]            -0.39808         0.45353     -0.00091779     -0.00065526
v  Velocity[Z]            -0.57766         0.18646      -0.0050036      -0.0039438
v  ǁVelocityǁ            0.20305          2.0008         0.97246         0.99889
v  Pressure               0.018916           2.911          2.5878          2.5898
v  TempC                     12.45          320.12          241.42          242.29
v  CourantNb                     1          2.0939          1.0004          1.0001
v  FourierNb             0.0053534         0.10983        0.021734        0.016646
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082596       0.0023837       0.0030639


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1357          1.0222          1.0168


 TIME FOR THE TIME STEP               66:        0.20468E+02

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


 INSTANT    0.670000000E+00   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53568E-01 0.17145E+00
   Friction velocity        uk    :  0.53568E-01 0.17145E+00
   Dimensionless distance   yplus :  0.24773E+01 0.14645E+02
   Friction thermal sca.    tstar :  0.74557E+00 0.65975E+02
   Rough dim-less th. sca.  tplus :  0.18483E+01 0.10927E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35102E-01      19   0.70012E-02   0.61806E-02 0.16484E+01 
c  Velocity[X]                                      0.50442E-02 
c  Velocity[Y]                                      0.55305E-03 
c  Velocity[Z]                                      0.58332E-03 
c  Pressure     0.68957E-04     610   0.27275E-02   0.16379E+00 0.11396E+01 
c  TempC        0.92257E+04      21   0.62913E-02   0.20733E+04 0.33929E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048072                          1523


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21852          1.9588         0.97116         0.99839
v  Velocity[Y]            -0.40019         0.45498      -0.0009196     -0.00066079
v  Velocity[Z]            -0.58087         0.18527      -0.0050339      -0.0039682
v  ǁVelocityǁ            0.22504          1.9945         0.97217          0.9989
v  Pressure             -0.0067247          2.9163           2.595           2.597
v  TempC                    14.148          326.05           240.7          241.46
v  CourantNb                     1          2.0802          1.0004          1.0001
v  FourierNb             0.0053528         0.11019        0.021746        0.016649
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082593       0.0023846       0.0030638


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054           2.122          1.0222          1.0168


 TIME FOR THE TIME STEP               67:        0.18296E+02

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


 INSTANT    0.680000000E+00   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53175E-01 0.17174E+00
   Friction velocity        uk    :  0.53175E-01 0.17174E+00
   Dimensionless distance   yplus :  0.30094E+01 0.14798E+02
   Friction thermal sca.    tstar :  0.69882E+00 0.65815E+02
   Rough dim-less th. sca.  tplus :  0.22453E+01 0.11041E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35112E-01      19   0.70500E-02   0.62922E-02 0.16635E+01 
c  Velocity[X]                                      0.51348E-02 
c  Velocity[Y]                                      0.57079E-03 
c  Velocity[Z]                                      0.58657E-03 
c  Pressure     0.74138E-04     684   0.31823E-02   0.17649E+00 0.24674E+01 
c  TempC        0.92056E+04      21   0.63564E-02   0.20442E+04 0.33784E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048003                          1517


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21976          1.9724         0.97086         0.99839
v  Velocity[Y]            -0.41295         0.45822     -0.00092409      -0.0006675
v  Velocity[Z]            -0.58519          0.1863      -0.0050644      -0.0039931
v  ǁVelocityǁ            0.22598            2.01         0.97187         0.99891
v  Pressure               0.010394          2.9303          2.6114          2.6134
v  TempC                     11.82          329.59          239.97          240.62
v  CourantNb                     1          2.0832          1.0004          1.0001
v  FourierNb             0.0053523         0.11057        0.021758        0.016652
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082591       0.0023855       0.0030637


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054           2.125          1.0222          1.0168


 TIME FOR THE TIME STEP               68:        0.18591E+02

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


 INSTANT    0.690000000E+00   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52625E-01 0.17212E+00
   Friction velocity        uk    :  0.52625E-01 0.17212E+00
   Dimensionless distance   yplus :  0.27781E+01 0.14624E+02
   Friction thermal sca.    tstar :  0.10640E+01 0.66210E+02
   Rough dim-less th. sca.  tplus :  0.20728E+01 0.10911E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35123E-01      19   0.69112E-02   0.62917E-02 0.16696E+01 
c  Velocity[X]                                      0.51232E-02 
c  Velocity[Y]                                      0.56106E-03 
c  Velocity[Z]                                      0.60749E-03 
c  Pressure     0.70070E-04     657   0.28233E-02   0.16718E+00 0.18361E+01 
c  TempC        0.91853E+04      21   0.64116E-02   0.20250E+04 0.33676E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048325                          1511


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20118          1.9775         0.97056          0.9984
v  Velocity[Y]            -0.41786         0.46197     -0.00092653     -0.00067403
v  Velocity[Z]            -0.58696         0.18534      -0.0050972      -0.0040184
v  ǁVelocityǁ            0.20227          2.0133         0.97158         0.99891
v  Pressure              0.0010732          2.9453          2.6236          2.6256
v  TempC                    9.1647          333.36          239.25          239.79
v  CourantNb                     1          2.0693          1.0004          1.0001
v  FourierNb              0.005352         0.11028         0.02177        0.016655
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082589       0.0023864       0.0030636


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1111          1.0222          1.0168


 TIME FOR THE TIME STEP               69:        0.19987E+02

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


 INSTANT    0.700000000E+00   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55831E-01 0.17242E+00
   Friction velocity        uk    :  0.55831E-01 0.17242E+00
   Dimensionless distance   yplus :  0.25266E+01 0.14828E+02
   Friction thermal sca.    tstar :  0.10311E+01 0.65985E+02
   Rough dim-less th. sca.  tplus :  0.18851E+01 0.11064E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35134E-01      19   0.67441E-02   0.59782E-02 0.16161E+01 
c  Velocity[X]                                      0.48478E-02 
c  Velocity[Y]                                      0.53678E-03 
c  Velocity[Z]                                      0.59356E-03 
c  Pressure     0.70450E-04     680   0.29925E-02   0.16831E+00 0.22595E+01 
c  TempC        0.91650E+04      21   0.64640E-02   0.20268E+04 0.33772E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048345                          1507


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20924          1.9808         0.97026          0.9984
v  Velocity[Y]            -0.42126         0.46592     -0.00093127     -0.00068186
v  Velocity[Z]            -0.59061         0.18559      -0.0051263      -0.0040402
v  ǁVelocityǁ            0.21082          2.0191         0.97129         0.99892
v  Pressure                0.01418          2.9554          2.6387          2.6408
v  TempC                    9.6979          334.86          238.53          238.96
v  CourantNb               0.99474          2.0685          1.0004          1.0001
v  FourierNb             0.0053517         0.11069        0.021783        0.016659
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001        0.008259       0.0023873       0.0030635


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1103          1.0222          1.0168


 TIME FOR THE TIME STEP               70:        0.18836E+02

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


 INSTANT    0.710000000E+00   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53610E-01 0.17241E+00
   Friction velocity        uk    :  0.53610E-01 0.17241E+00
   Dimensionless distance   yplus :  0.29714E+01 0.14629E+02
   Friction thermal sca.    tstar :  0.97584E+00 0.65499E+02
   Rough dim-less th. sca.  tplus :  0.22170E+01 0.10915E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35145E-01      19   0.67679E-02   0.60494E-02 0.16235E+01 
c  Velocity[X]                                      0.49364E-02 
c  Velocity[Y]                                      0.54248E-03 
c  Velocity[Z]                                      0.57056E-03 
c  Pressure     0.68429E-04     626   0.27210E-02   0.16370E+00 0.14076E+01 
c  TempC        0.91447E+04      21   0.63655E-02   0.20028E+04 0.33634E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048105                          1502


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.19235          1.9832         0.96997          0.9984
v  Velocity[Y]            -0.41913         0.46128     -0.00093366     -0.00068702
v  Velocity[Z]            -0.58987         0.19226      -0.0051562      -0.0040631
v  ǁVelocityǁ            0.19393          2.0187           0.971         0.99893
v  Pressure             -0.0049347          2.9687           2.648          2.6501
v  TempC                    14.563          336.42          237.81          238.12
v  CourantNb                     1          2.0788          1.0004          1.0001
v  FourierNb             0.0053514         0.11143        0.021795        0.016662
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082588       0.0023882       0.0030634


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1206          1.0222          1.0168


 TIME FOR THE TIME STEP               71:        0.20209E+02

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


 INSTANT    0.720000000E+00   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.47808E-01 0.17288E+00
   Friction velocity        uk    :  0.47808E-01 0.17288E+00
   Dimensionless distance   yplus :  0.27560E+01 0.14884E+02
   Friction thermal sca.    tstar :  0.91470E+00 0.65872E+02
   Rough dim-less th. sca.  tplus :  0.20563E+01 0.11105E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35155E-01      19   0.68108E-02   0.59691E-02 0.16155E+01 
c  Velocity[X]                                      0.48659E-02 
c  Velocity[Y]                                      0.53749E-03 
c  Velocity[Z]                                      0.56577E-03 
c  Pressure     0.71864E-04     716   0.30989E-02   0.17201E+00 0.23918E+01 
c  TempC        0.91243E+04      21   0.64908E-02   0.19818E+04 0.33513E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048213                          1501


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              0.1867          1.9901         0.96968         0.99841
v  Velocity[Y]            -0.42507         0.45985     -0.00093705     -0.00069339
v  Velocity[Z]            -0.59501         0.18725      -0.0051857      -0.0040852
v  ǁVelocityǁ            0.18839           2.028         0.97071         0.99894
v  Pressure               0.007703          2.9848          2.6643          2.6663
v  TempC                    11.365          337.13          237.09          237.29
v  CourantNb                     1          2.0741          1.0004          1.0001
v  FourierNb              0.005351         0.11195        0.021807        0.016665
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082586       0.0023891       0.0030633


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1159          1.0222          1.0168


 TIME FOR THE TIME STEP               72:        0.19250E+02

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


 INSTANT    0.730000000E+00   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52006E-01 0.17292E+00
   Friction velocity        uk    :  0.52006E-01 0.17292E+00
   Dimensionless distance   yplus :  0.23535E+01 0.14677E+02
   Friction thermal sca.    tstar :  0.85226E+00 0.64435E+02
   Rough dim-less th. sca.  tplus :  0.17560E+01 0.10951E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35166E-01      19   0.67898E-02   0.58646E-02 0.16058E+01 
c  Velocity[X]                                      0.47928E-02 
c  Velocity[Y]                                      0.51497E-03 
c  Velocity[Z]                                      0.55688E-03 
c  Pressure     0.68192E-04     660   0.28230E-02   0.16339E+00 0.19788E+01 
c  TempC        0.91039E+04      21   0.65533E-02   0.19751E+04 0.33538E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048545                          1496


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.19758          1.9944         0.96939         0.99841
v  Velocity[Y]             -0.4306         0.46073      -0.0009404     -0.00070029
v  Velocity[Z]            -0.59687         0.18338      -0.0052143      -0.0041063
v  ǁVelocityǁ            0.20229          2.0301         0.97043         0.99895
v  Pressure            -0.00095647          2.9981          2.6777          2.6798
v  TempC                    9.8057          335.02          236.37          236.46
v  CourantNb                     1          2.0599          1.0004          1.0001
v  FourierNb             0.0053507         0.11205        0.021819        0.016669
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082588         0.00239       0.0030632


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1017          1.0222          1.0168


 TIME FOR THE TIME STEP               73:        0.18161E+02

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


 INSTANT    0.740000000E+00   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54133E-01 0.17326E+00
   Friction velocity        uk    :  0.54133E-01 0.17326E+00
   Dimensionless distance   yplus :  0.29266E+01 0.14887E+02
   Friction thermal sca.    tstar :  0.79233E+00 0.62881E+02
   Rough dim-less th. sca.  tplus :  0.21836E+01 0.11107E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35176E-01      19   0.68130E-02   0.60643E-02 0.16253E+01 
c  Velocity[X]                                      0.49687E-02 
c  Velocity[Y]                                      0.53338E-03 
c  Velocity[Z]                                      0.56216E-03 
c  Pressure     0.71942E-04     681   0.30893E-02   0.17278E+00 0.22450E+01 
c  TempC        0.90834E+04      21   0.66455E-02   0.19621E+04 0.33529E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048497                          1496


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.19187          2.0042          0.9691         0.99842
v  Velocity[Y]            -0.43382         0.46436     -0.00094517     -0.00070719
v  Velocity[Z]            -0.60262         0.18259      -0.0052377       -0.004125
v  ǁVelocityǁ            0.19605          2.0424         0.97014         0.99896
v  Pressure               0.020416          3.0144          2.6931          2.6952
v  TempC                    4.6749          318.97          235.65          235.63
v  CourantNb               0.97919           2.062          1.0004          1.0001
v  FourierNb             0.0053504         0.11167        0.021831        0.016672
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082586       0.0023909       0.0030632


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1038          1.0223          1.0168


 TIME FOR THE TIME STEP               74:        0.18775E+02

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


 INSTANT    0.750000000E+00   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53456E-01 0.17354E+00
   Friction velocity        uk    :  0.53456E-01 0.17354E+00
   Dimensionless distance   yplus :  0.27301E+01 0.14711E+02
   Friction thermal sca.    tstar :  0.73629E+00 0.61868E+02
   Rough dim-less th. sca.  tplus :  0.20369E+01 0.10976E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         75, Physical time    0.75000E+00


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
 End writing


 Time for restart files:    0.13700E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35187E-01      19   0.66887E-02   0.60050E-02 0.16206E+01 
c  Velocity[X]                                      0.48938E-02 
c  Velocity[Y]                                      0.53421E-03 
c  Velocity[Z]                                      0.57700E-03 
c  Pressure     0.68671E-04     606   0.26860E-02   0.16525E+00 0.98342E+00 
c  TempC        0.90629E+04      21   0.65579E-02   0.19501E+04 0.33513E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048361                          1496


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              0.1837          2.0067         0.96881         0.99842
v  Velocity[Y]            -0.43337         0.46398     -0.00094689     -0.00071282
v  Velocity[Z]            -0.60944         0.18169      -0.0052632      -0.0041449
v  ǁVelocityǁ            0.18885          2.0427         0.96986         0.99896
v  Pressure              0.0089487          3.0208          2.6995          2.7016
v  TempC                    2.4806          322.67          234.94           234.8
v  CourantNb                     1          2.0678          1.0004          1.0001
v  FourierNb               0.00535         0.11102        0.021843        0.016675
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082584       0.0023917       0.0030631


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0054          2.1096          1.0223          1.0168


 TIME FOR THE TIME STEP               75:        0.17734E+02

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


 INSTANT    0.760000000E+00   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52597E-01 0.17379E+00
   Friction velocity        uk    :  0.52597E-01 0.17379E+00
   Dimensionless distance   yplus :  0.24784E+01 0.14932E+02
   Friction thermal sca.    tstar :  0.68499E+00 0.61712E+02
   Rough dim-less th. sca.  tplus :  0.18492E+01 0.11141E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35198E-01      19   0.67773E-02   0.58072E-02 0.15876E+01 
c  Velocity[X]                                      0.47287E-02 
c  Velocity[Y]                                      0.53228E-03 
c  Velocity[Z]                                      0.54619E-03 
c  Pressure     0.68492E-04     628   0.27370E-02   0.16510E+00 0.12198E+01 
c  TempC        0.90424E+04      21   0.63668E-02   0.19282E+04 0.33359E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048653                          1495


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.18409          2.0043         0.96852         0.99842
v  Velocity[Y]             -0.4194         0.46444     -0.00094988     -0.00071919
v  Velocity[Z]             -0.6023         0.18977      -0.0052884       -0.004164
v  ǁVelocityǁ            0.18783          2.0422         0.96958         0.99897
v  Pressure              0.0080087          3.0287          2.7077          2.7098
v  TempC                    1.9405          318.87          234.22          233.97
v  CourantNb                     1          2.0554          1.0004          1.0001
v  FourierNb             0.0053496         0.11177        0.021856        0.016679
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082585       0.0023926        0.003063


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0972          1.0223          1.0168


 TIME FOR THE TIME STEP               76:        0.17556E+02

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


 INSTANT    0.770000000E+00   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52587E-01 0.17382E+00
   Friction velocity        uk    :  0.52587E-01 0.17382E+00
   Dimensionless distance   yplus :  0.29874E+01 0.14735E+02
   Friction thermal sca.    tstar :  0.70226E+00 0.62192E+02
   Rough dim-less th. sca.  tplus :  0.22290E+01 0.10994E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35208E-01      19   0.67552E-02   0.58722E-02 0.15986E+01 
c  Velocity[X]                                      0.47917E-02 
c  Velocity[Y]                                      0.51263E-03 
c  Velocity[Z]                                      0.56784E-03 
c  Pressure     0.68310E-04     645   0.28020E-02   0.16491E+00 0.15353E+01 
c  TempC        0.90218E+04      21   0.63998E-02   0.19039E+04 0.33242E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048778                          1492


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.18149          2.0126         0.96823         0.99843
v  Velocity[Y]            -0.42525         0.46807      -0.0009536     -0.00072515
v  Velocity[Z]            -0.60634         0.18163      -0.0053133      -0.0041834
v  ǁVelocityǁ            0.18567          2.0478         0.96929         0.99898
v  Pressure             -0.0024035          3.0376          2.7182          2.7203
v  TempC                    2.0199          319.35          233.51          233.14
v  CourantNb               0.99966          2.0501          1.0004          1.0001
v  FourierNb             0.0053492         0.11256        0.021868        0.016682
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082585       0.0023935       0.0030629


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0919          1.0223          1.0168


 TIME FOR THE TIME STEP               77:        0.17626E+02

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


 INSTANT    0.780000000E+00   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52294E-01 0.17409E+00
   Friction velocity        uk    :  0.52294E-01 0.17409E+00
   Dimensionless distance   yplus :  0.27057E+01 0.14963E+02
   Friction thermal sca.    tstar :  0.10432E+01 0.62580E+02
   Rough dim-less th. sca.  tplus :  0.20188E+01 0.11164E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35218E-01      19   0.66871E-02   0.58128E-02 0.15884E+01 
c  Velocity[X]                                      0.47223E-02 
c  Velocity[Y]                                      0.52257E-03 
c  Velocity[Z]                                      0.56790E-03 
c  Pressure     0.70511E-04     664   0.30276E-02   0.17038E+00 0.20989E+01 
c  TempC        0.90013E+04      21   0.65896E-02   0.18839E+04 0.33121E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048435                          1492


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.17598          2.0178         0.96795         0.99843
v  Velocity[Y]            -0.42684          0.4687     -0.00095653      -0.0007316
v  Velocity[Z]            -0.61095          0.1816       -0.005338      -0.0042014
v  ǁVelocityǁ            0.18065          2.0553         0.96901         0.99899
v  Pressure               0.015178           3.054          2.7328          2.7349
v  TempC                    4.3836          321.91           232.8          232.31
v  CourantNb                     1          2.0646          1.0004          1.0001
v  FourierNb             0.0053488         0.11247         0.02188        0.016685
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082585       0.0023944       0.0030629


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.1064          1.0223          1.0168


 TIME FOR THE TIME STEP               78:        0.18223E+02

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


 INSTANT    0.790000000E+00   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51661E-01 0.17408E+00
   Friction velocity        uk    :  0.51661E-01 0.17408E+00
   Dimensionless distance   yplus :  0.24064E+01 0.14763E+02
   Friction thermal sca.    tstar :  0.10048E+01 0.63339E+02
   Rough dim-less th. sca.  tplus :  0.17955E+01 0.11015E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35229E-01      19   0.66888E-02   0.58573E-02 0.15963E+01 
c  Velocity[X]                                      0.47683E-02 
c  Velocity[Y]                                      0.52744E-03 
c  Velocity[Z]                                      0.56162E-03 
c  Pressure     0.68654E-04     611   0.27554E-02   0.16610E+00 0.11757E+01 
c  TempC        0.89806E+04      21   0.67954E-02   0.18779E+04 0.33145E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048736                          1489


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.17511          2.0242         0.96766         0.99843
v  Velocity[Y]            -0.43533         0.46734      -0.0009616     -0.00073869
v  Velocity[Z]            -0.61166         0.18122      -0.0053578       -0.004217
v  ǁVelocityǁ            0.18055          2.0597         0.96874         0.99899
v  Pressure              0.0074342          3.0624          2.7408          2.7429
v  TempC                   0.27386          324.25          232.09          231.48
v  CourantNb                     1          2.0519          1.0004          1.0001
v  FourierNb             0.0053484         0.11252        0.021892        0.016689
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082586       0.0023953       0.0030628


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0936          1.0223          1.0168


 TIME FOR THE TIME STEP               79:        0.18273E+02

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


 INSTANT    0.800000000E+00   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51559E-01 0.17433E+00
   Friction velocity        uk    :  0.51559E-01 0.17433E+00
   Dimensionless distance   yplus :  0.29287E+01 0.14973E+02
   Friction thermal sca.    tstar :  0.93726E+00 0.63179E+02
   Rough dim-less th. sca.  tplus :  0.21851E+01 0.11171E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35239E-01      19   0.66754E-02   0.57778E-02 0.15924E+01 
c  Velocity[X]                                      0.47021E-02 
c  Velocity[Y]                                      0.52284E-03 
c  Velocity[Z]                                      0.55289E-03 
c  Pressure     0.68453E-04     644   0.27849E-02   0.16569E+00 0.13784E+01 
c  TempC        0.89599E+04      21   0.65726E-02   0.18642E+04 0.33072E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048886                          1485


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.17201          2.0248         0.96738         0.99844
v  Velocity[Y]            -0.44184          0.4684     -0.00096664     -0.00074611
v  Velocity[Z]            -0.60224         0.19112      -0.0053815      -0.0042342
v  ǁVelocityǁ            0.17758          2.0623         0.96846           0.999
v  Pressure               0.010598          3.0709          2.7502          2.7524
v  TempC                    6.0604          325.56          231.38          230.65
v  CourantNb                     1          2.0456          1.0004          1.0001
v  FourierNb              0.005348         0.11205        0.021904        0.016692
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082584       0.0023962       0.0030627


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0874          1.0223          1.0168


 TIME FOR THE TIME STEP               80:        0.19499E+02

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


 INSTANT    0.810000000E+00   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51167E-01 0.17450E+00
   Friction velocity        uk    :  0.51167E-01 0.17450E+00
   Dimensionless distance   yplus :  0.27333E+01 0.14801E+02
   Friction thermal sca.    tstar :  0.86233E+00 0.62740E+02
   Rough dim-less th. sca.  tplus :  0.20394E+01 0.11043E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35250E-01      19   0.66691E-02   0.56189E-02 0.15653E+01 
c  Velocity[X]                                      0.45692E-02 
c  Velocity[Y]                                      0.50450E-03 
c  Velocity[Z]                                      0.54521E-03 
c  Pressure     0.66712E-04     629   0.27022E-02   0.16151E+00 0.11861E+01 
c  TempC        0.89391E+04      21   0.67226E-02   0.18463E+04 0.33020E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048689                          1483


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.16465          2.0266          0.9671         0.99844
v  Velocity[Y]            -0.44466         0.47029     -0.00096855     -0.00075257
v  Velocity[Z]            -0.60335          0.1833      -0.0054045      -0.0042515
v  ǁVelocityǁ            0.17081          2.0617         0.96819         0.99901
v  Pressure             -0.0030114          3.0788          2.7583          2.7605
v  TempC                    6.3233          323.58          230.67          229.82
v  CourantNb               0.99828          2.0539          1.0004          1.0001
v  FourierNb             0.0053477          0.1121        0.021916        0.016695
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082583       0.0023971       0.0030627


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0956          1.0223          1.0168


 TIME FOR THE TIME STEP               81:        0.17337E+02

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


 INSTANT    0.820000000E+00   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50326E-01 0.17436E+00
   Friction velocity        uk    :  0.50326E-01 0.17436E+00
   Dimensionless distance   yplus :  0.24945E+01 0.15013E+02
   Friction thermal sca.    tstar :  0.80289E+00 0.63048E+02
   Rough dim-less th. sca.  tplus :  0.18612E+01 0.11202E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35260E-01      19   0.65862E-02   0.58060E-02 0.15882E+01 
c  Velocity[X]                                      0.47123E-02 
c  Velocity[Y]                                      0.53190E-03 
c  Velocity[Z]                                      0.56172E-03 
c  Pressure     0.70627E-04     675   0.30477E-02   0.17165E+00 0.19066E+01 
c  TempC        0.89184E+04      21   0.67895E-02   0.18392E+04 0.33037E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048722                          1486


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.15775          2.0298         0.96682         0.99844
v  Velocity[Y]            -0.44434         0.47141     -0.00097571     -0.00076168
v  Velocity[Z]            -0.60754         0.18112      -0.0054247       -0.004267
v  ǁVelocityǁ            0.16293          2.0676         0.96791         0.99902
v  Pressure               0.012542          3.0952          2.7718          2.7739
v  TempC                    3.3855          320.32          229.96             229
v  CourantNb                     1          2.0525          1.0004          1.0001
v  FourierNb             0.0053474         0.11206        0.021929        0.016699
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082583        0.002398       0.0030626


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0943          1.0223          1.0168


 TIME FOR THE TIME STEP               82:        0.18411E+02

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


 INSTANT    0.830000000E+00   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49496E-01 0.17428E+00
   Friction velocity        uk    :  0.49496E-01 0.17428E+00
   Dimensionless distance   yplus :  0.29323E+01 0.14803E+02
   Friction thermal sca.    tstar :  0.79908E+00 0.62698E+02
   Rough dim-less th. sca.  tplus :  0.21878E+01 0.11044E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35270E-01      19   0.66580E-02   0.56671E-02 0.15655E+01 
c  Velocity[X]                                      0.46152E-02 
c  Velocity[Y]                                      0.50655E-03 
c  Velocity[Z]                                      0.54544E-03 
c  Pressure     0.67206E-04     646   0.27663E-02   0.16356E+00 0.15910E+01 
c  TempC        0.88976E+04      21   0.69665E-02   0.18106E+04 0.32834E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step       0.0004888                          1485


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.15073          2.0353         0.96655         0.99845
v  Velocity[Y]            -0.44642         0.46973     -0.00098076     -0.00076861
v  Velocity[Z]            -0.60858          0.1799      -0.0054459      -0.0042822
v  ǁVelocityǁ            0.15683          2.0711         0.96764         0.99902
v  Pressure               0.006329          3.1031           2.783          2.7851
v  TempC                    1.6261          320.68          229.25          228.17
v  CourantNb                     1          2.0458          1.0004          1.0001
v  FourierNb              0.005347         0.11273        0.021941        0.016702
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082578       0.0023989       0.0030625


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0876          1.0224          1.0168


 TIME FOR THE TIME STEP               83:        0.17616E+02

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


 INSTANT    0.840000000E+00   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48667E-01 0.17462E+00
   Friction velocity        uk    :  0.48667E-01 0.17462E+00
   Dimensionless distance   yplus :  0.27348E+01 0.15038E+02
   Friction thermal sca.    tstar :  0.74861E+00 0.62876E+02
   Rough dim-less th. sca.  tplus :  0.20404E+01 0.11220E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35280E-01      19   0.65276E-02   0.56044E-02 0.15550E+01 
c  Velocity[X]                                      0.45618E-02 
c  Velocity[Y]                                      0.50389E-03 
c  Velocity[Z]                                      0.53875E-03 
c  Pressure     0.68360E-04     647   0.28938E-02   0.16650E+00 0.15458E+01 
c  TempC        0.88767E+04      21   0.69120E-02   0.18123E+04 0.32959E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048562                          1486


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.15512          2.0332         0.96627         0.99845
v  Velocity[Y]            -0.45186         0.47278     -0.00098326     -0.00077516
v  Velocity[Z]            -0.60875         0.18987      -0.0054657      -0.0042967
v  ǁVelocityǁ            0.16074          2.0706         0.96737         0.99903
v  Pressure              0.0082174          3.1132          2.7939           2.796
v  TempC                    4.5866          321.61          228.54          227.34
v  CourantNb               0.98058          2.0592          1.0004          1.0001
v  FourierNb             0.0053466         0.11292        0.021952        0.016705
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001        0.008258       0.0023997       0.0030625


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053           2.101          1.0224          1.0168


 TIME FOR THE TIME STEP               84:        0.17581E+02

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


 INSTANT    0.850000000E+00   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49248E-01 0.17479E+00
   Friction velocity        uk    :  0.49248E-01 0.17479E+00
   Dimensionless distance   yplus :  0.24108E+01 0.14859E+02
   Friction thermal sca.    tstar :  0.70062E+00 0.63243E+02
   Rough dim-less th. sca.  tplus :  0.17987E+01 0.11087E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35291E-01      19   0.65365E-02   0.55308E-02 0.15385E+01 
c  Velocity[X]                                      0.44904E-02 
c  Velocity[Y]                                      0.49496E-03 
c  Velocity[Z]                                      0.54550E-03 
c  Pressure     0.67099E-04     628   0.27723E-02   0.16371E+00 0.14595E+01 
c  TempC        0.88558E+04      21   0.67763E-02   0.18131E+04 0.33020E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048653                          1483


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.15519          2.0408           0.966         0.99845
v  Velocity[Y]            -0.45418         0.46976     -0.00098738     -0.00078302
v  Velocity[Z]            -0.61399         0.17961      -0.0054855      -0.0043115
v  ǁVelocityǁ            0.16049          2.0763         0.96711         0.99904
v  Pressure             -0.0025268          3.1266          2.8042          2.8063
v  TempC                  -0.95924          324.69          227.84          226.52
v  CourantNb                     1          2.0554          1.0004          1.0001
v  FourierNb             0.0053462         0.11357        0.021964        0.016709
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001        0.008258       0.0024006       0.0030624


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0971          1.0224          1.0168


 TIME FOR THE TIME STEP               85:        0.17125E+02

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


 INSTANT    0.860000000E+00   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48225E-01 0.17517E+00
   Friction velocity        uk    :  0.48225E-01 0.17517E+00
   Dimensionless distance   yplus :  0.29292E+01 0.15062E+02
   Friction thermal sca.    tstar :  0.90965E+00 0.63400E+02
   Rough dim-less th. sca.  tplus :  0.21855E+01 0.11238E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35300E-01      19   0.66409E-02   0.56286E-02 0.15540E+01 
c  Velocity[X]                                      0.45895E-02 
c  Velocity[Y]                                      0.50025E-03 
c  Velocity[Z]                                      0.53889E-03 
c  Pressure     0.70168E-04     679   0.30901E-02   0.17137E+00 0.22487E+01 
c  TempC        0.88348E+04      21   0.66131E-02   0.17857E+04 0.32841E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048885                          1484


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.15569          2.0439         0.96573         0.99846
v  Velocity[Y]            -0.45457         0.46662     -0.00099286     -0.00079129
v  Velocity[Z]            -0.61501         0.17922      -0.0055054      -0.0043257
v  ǁVelocityǁ             0.1609           2.082         0.96684         0.99904
v  Pressure               0.013219          3.1433          2.8204          2.8225
v  TempC                    6.8745          321.63          227.13          225.69
v  CourantNb                     1          2.0456          1.0004          1.0001
v  FourierNb             0.0053458         0.11316        0.021977        0.016712
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001        0.008258       0.0024015       0.0030624


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0874          1.0224          1.0168


 TIME FOR THE TIME STEP               86:        0.18941E+02

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


 INSTANT    0.870000000E+00   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49204E-01 0.17515E+00
   Friction velocity        uk    :  0.49204E-01 0.17515E+00
   Dimensionless distance   yplus :  0.27575E+01 0.14865E+02
   Friction thermal sca.    tstar :  0.86466E+00 0.61013E+02
   Rough dim-less th. sca.  tplus :  0.20574E+01 0.11091E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35311E-01      19   0.65656E-02   0.56682E-02 0.15766E+01 
c  Velocity[X]                                      0.46177E-02 
c  Velocity[Y]                                      0.51112E-03 
c  Velocity[Z]                                      0.53929E-03 
c  Pressure     0.67610E-04     628   0.27535E-02   0.16541E+00 0.13764E+01 
c  TempC        0.88139E+04      21   0.68436E-02   0.17548E+04 0.32614E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048997                          1482


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.14915          2.0481         0.96546         0.99846
v  Velocity[Y]               -0.44         0.46779     -0.00099813     -0.00079909
v  Velocity[Z]            -0.61987         0.17829      -0.0055244      -0.0043401
v  ǁVelocityǁ            0.15629          2.0841         0.96658         0.99905
v  Pressure              0.0064717          3.1491          2.8302          2.8323
v  TempC                   0.80662          321.68          226.43          224.87
v  CourantNb                     1          2.0409          1.0004          1.0001
v  FourierNb             0.0053455         0.11331        0.021988        0.016716
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001        0.008258       0.0024024       0.0030623


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0827          1.0224          1.0168


 TIME FOR THE TIME STEP               87:        0.17609E+02

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


 INSTANT    0.880000000E+00   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48417E-01 0.17534E+00
   Friction velocity        uk    :  0.48417E-01 0.17534E+00
   Dimensionless distance   yplus :  0.25051E+01 0.15080E+02
   Friction thermal sca.    tstar :  0.83755E+00 0.61109E+02
   Rough dim-less th. sca.  tplus :  0.18691E+01 0.11252E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35321E-01      19   0.64406E-02   0.55589E-02 0.15468E+01 
c  Velocity[X]                                      0.45272E-02 
c  Velocity[Y]                                      0.49147E-03 
c  Velocity[Z]                                      0.54025E-03 
c  Pressure     0.68340E-04     666   0.28652E-02   0.16754E+00 0.16061E+01 
c  TempC        0.87928E+04      21   0.69213E-02   0.17521E+04 0.32644E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048608                          1478


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.14916          2.0522         0.96519         0.99846
v  Velocity[Y]            -0.44561         0.46684      -0.0010032     -0.00080769
v  Velocity[Z]            -0.61385         0.18965      -0.0055417      -0.0043519
v  ǁVelocityǁ            0.15522          2.0905         0.96631         0.99906
v  Pressure               0.023115            3.16          2.8417          2.8439
v  TempC                   -5.1342          321.64          225.73          224.04
v  CourantNb               0.97707          2.0573          1.0004          1.0001
v  FourierNb             0.0053451         0.11319        0.022001        0.016719
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082579       0.0024033       0.0030623


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0991          1.0224          1.0169


 TIME FOR THE TIME STEP               88:        0.18255E+02

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


 INSTANT    0.890000000E+00   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447994E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48423E-01 0.17535E+00
   Friction velocity        uk    :  0.48423E-01 0.17535E+00
   Dimensionless distance   yplus :  0.29209E+01 0.14878E+02
   Friction thermal sca.    tstar :  0.80926E+00 0.60006E+02
   Rough dim-less th. sca.  tplus :  0.21793E+01 0.11101E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35331E-01      19   0.64460E-02   0.52895E-02 0.15073E+01 
c  Velocity[X]                                      0.42743E-02 
c  Velocity[Y]                                      0.49090E-03 
c  Velocity[Z]                                      0.52426E-03 
c  Pressure     0.64996E-04     548   0.25881E-02   0.15922E+00 0.71590E+00 
c  TempC        0.87717E+04      21   0.69820E-02   0.17413E+04 0.32654E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048847                          1481


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.14511          2.0514         0.96493         0.99847
v  Velocity[Y]            -0.44461         0.46917      -0.0010077     -0.00081573
v  Velocity[Z]            -0.61419         0.17805      -0.0055595      -0.0043649
v  ǁVelocityǁ            0.15095          2.0871         0.96605         0.99907
v  Pressure            -0.00069765           3.169          2.8465          2.8487
v  TempC                   -3.8492          323.07          225.03          223.22
v  CourantNb                     1          2.0472          1.0004          1.0001
v  FourierNb             0.0053447         0.11304        0.022012        0.016722
v  total_pressure      1.0132e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082578       0.0024041       0.0030622


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053           2.089          1.0224          1.0169


 TIME FOR THE TIME STEP               89:        0.17205E+02

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


 INSTANT    0.900000000E+00   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.47902E-01 0.17577E+00
   Friction velocity        uk    :  0.47902E-01 0.17577E+00
   Dimensionless distance   yplus :  0.26516E+01 0.15117E+02
   Friction thermal sca.    tstar :  0.78965E+00 0.59365E+02
   Rough dim-less th. sca.  tplus :  0.19784E+01 0.11279E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35341E-01      19   0.65593E-02   0.54627E-02 0.15305E+01 
c  Velocity[X]                                      0.44401E-02 
c  Velocity[Y]                                      0.49558E-03 
c  Velocity[Z]                                      0.52698E-03 
c  Pressure     0.70208E-04     675   0.30071E-02   0.17232E+00 0.17121E+01 
c  TempC        0.87505E+04      21   0.68706E-02   0.17361E+04 0.32688E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048949                          1482


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              0.1326          2.0593         0.96466         0.99847
v  Velocity[Y]            -0.45312         0.47356      -0.0010128     -0.00082355
v  Velocity[Z]            -0.61636         0.17806      -0.0055741       -0.004376
v  ǁVelocityǁ            0.13938          2.0974         0.96579         0.99907
v  Pressure               0.016462          3.1818          2.8589          2.8611
v  TempC                   -1.4057          325.77          224.33          222.39
v  CourantNb                     1           2.043          1.0004          1.0001
v  FourierNb             0.0053443         0.11357        0.022025        0.016726
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082579        0.002405       0.0030622


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0847          1.0224          1.0169


 TIME FOR THE TIME STEP               90:        0.18057E+02

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


 INSTANT    0.910000000E+00   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.46335E-01 0.17573E+00
   Friction velocity        uk    :  0.46335E-01 0.17573E+00
   Dimensionless distance   yplus :  0.23264E+01 0.14907E+02
   Friction thermal sca.    tstar :  0.77372E+00 0.58740E+02
   Rough dim-less th. sca.  tplus :  0.17357E+01 0.11122E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35351E-01      19   0.64656E-02   0.53938E-02 0.15207E+01 
c  Velocity[X]                                      0.43721E-02 
c  Velocity[Y]                                      0.49579E-03 
c  Velocity[Z]                                      0.52586E-03 
c  Pressure     0.66166E-04     610   0.26852E-02   0.16262E+00 0.10766E+01 
c  TempC        0.87293E+04      21   0.71125E-02   0.17165E+04 0.32532E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048666                          1485


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.21207          2.0633          0.9644         0.99847
v  Velocity[Y]            -0.45722         0.47444       -0.001021     -0.00083345
v  Velocity[Z]            -0.62182          0.1761       -0.005589      -0.0043864
v  ǁVelocityǁ            0.21594          2.0993         0.96553         0.99908
v  Pressure              0.0073076          3.1899          2.8666          2.8688
v  TempC                   -7.0567           321.9          223.63          221.57
v  CourantNb                     1          2.0548          1.0004          1.0001
v  FourierNb             0.0053438         0.11409        0.022037        0.016729
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0082574       0.0024059       0.0030622


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0966          1.0225          1.0169


 TIME FOR THE TIME STEP               91:        0.17057E+02

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


 INSTANT    0.920000000E+00   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52190E-01 0.17589E+00
   Friction velocity        uk    :  0.52190E-01 0.17589E+00
   Dimensionless distance   yplus :  0.28849E+01 0.15112E+02
   Friction thermal sca.    tstar :  0.73910E+00 0.58069E+02
   Rough dim-less th. sca.  tplus :  0.21525E+01 0.11275E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35361E-01      19   0.64791E-02   0.54211E-02 0.15273E+01 
c  Velocity[X]                                      0.44177E-02 
c  Velocity[Y]                                      0.48142E-03 
c  Velocity[Z]                                      0.52193E-03 
c  Pressure     0.67588E-04     649   0.28455E-02   0.16632E+00 0.13687E+01 
c  TempC        0.87080E+04      21   0.71229E-02   0.17110E+04 0.32563E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048583                          1484


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.20178          2.0676         0.96413         0.99848
v  Velocity[Y]             -0.4607         0.47844      -0.0010271     -0.00084259
v  Velocity[Z]            -0.61782         0.18952      -0.0056049      -0.0043982
v  ǁVelocityǁ            0.20487           2.106         0.96527         0.99908
v  Pressure               0.025721          3.1978          2.8765          2.8787
v  TempC                    -15.67          324.55          222.93          220.75
v  CourantNb                     1          2.0583          1.0004          1.0001
v  FourierNb             0.0053434         0.11407        0.022049        0.016733
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0083838       0.0024068       0.0030621


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.1001          1.0225          1.0169


 TIME FOR THE TIME STEP               92:        0.18471E+02

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


 INSTANT    0.930000000E+00   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51938E-01 0.17589E+00
   Friction velocity        uk    :  0.51938E-01 0.17589E+00
   Dimensionless distance   yplus :  0.27299E+01 0.14932E+02
   Friction thermal sca.    tstar :  0.68838E+00 0.58445E+02
   Rough dim-less th. sca.  tplus :  0.20368E+01 0.11141E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35371E-01      19   0.64267E-02   0.53564E-02 0.15250E+01 
c  Velocity[X]                                      0.43560E-02 
c  Velocity[Y]                                      0.48300E-03 
c  Velocity[Z]                                      0.51733E-03 
c  Pressure     0.65276E-04     515   0.26114E-02   0.16071E+00 0.49672E+00 
c  TempC        0.86867E+04      21   0.70173E-02   0.16947E+04 0.32468E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048875                          1487


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.17261          2.0644         0.96387         0.99848
v  Velocity[Y]            -0.45761         0.47742      -0.0010332     -0.00085177
v  Velocity[Z]            -0.62416         0.17776      -0.0056204      -0.0044095
v  ǁVelocityǁ            0.17359          2.1002         0.96501         0.99909
v  Pressure              0.0043958          3.2001          2.8794          2.8816
v  TempC                   -6.2861          326.66          222.23          219.93
v  CourantNb                     1           2.046          1.0004          1.0001
v  FourierNb             0.0053429         0.11396         0.02206        0.016736
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0084956       0.0024077       0.0030621


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0878          1.0225          1.0169


 TIME FOR THE TIME STEP               93:        0.16165E+02

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


 INSTANT    0.940000000E+00   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49395E-01 0.17611E+00
   Friction velocity        uk    :  0.49395E-01 0.17611E+00
   Dimensionless distance   yplus :  0.24656E+01 0.15156E+02
   Friction thermal sca.    tstar :  0.80304E+00 0.59525E+02
   Rough dim-less th. sca.  tplus :  0.18396E+01 0.11308E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35381E-01      19   0.63732E-02   0.53765E-02 0.15162E+01 
c  Velocity[X]                                      0.43752E-02 
c  Velocity[Y]                                      0.47625E-03 
c  Velocity[Z]                                      0.52507E-03 
c  Pressure     0.68905E-04     664   0.29198E-02   0.16994E+00 0.13390E+01 
c  TempC        0.86653E+04      21   0.68890E-02   0.16840E+04 0.32499E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00049013                          1485


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.17474          2.0717         0.96361         0.99848
v  Velocity[Y]            -0.45833          0.4799      -0.0010388     -0.00086114
v  Velocity[Z]            -0.62587         0.18971      -0.0056366      -0.0044204
v  ǁVelocityǁ            0.17811          2.1097         0.96476          0.9991
v  Pressure               0.021026            3.21          2.8891          2.8913
v  TempC                   -11.674          322.41          221.54          219.11
v  CourantNb                     1          2.0403          1.0004          1.0001
v  FourierNb             0.0053426         0.11406        0.022073         0.01674
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0086303       0.0024086        0.003062


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0821          1.0225          1.0169


 TIME FOR THE TIME STEP               94:        0.18718E+02

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


 INSTANT    0.950000000E+00   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50896E-01 0.17618E+00
   Friction velocity        uk    :  0.50896E-01 0.17618E+00
   Dimensionless distance   yplus :  0.29575E+01 0.14947E+02
   Friction thermal sca.    tstar :  0.80227E+00 0.59934E+02
   Rough dim-less th. sca.  tplus :  0.22066E+01 0.11152E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35391E-01      19   0.64087E-02   0.53016E-02 0.15048E+01 
c  Velocity[X]                                      0.42845E-02 
c  Velocity[Y]                                      0.48747E-03 
c  Velocity[Z]                                      0.52965E-03 
c  Pressure     0.65571E-04     578   0.26582E-02   0.16195E+00 0.85913E+00 
c  TempC        0.86439E+04      21   0.70185E-02   0.16521E+04 0.32194E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048761                          1487


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.16136          2.0727         0.96335         0.99849
v  Velocity[Y]            -0.45047         0.47916       -0.001045     -0.00086964
v  Velocity[Z]            -0.62491         0.17908      -0.0056492      -0.0044296
v  ǁVelocityǁ            0.16595          2.1085          0.9645         0.99911
v  Pressure              0.0093962          3.2193          2.8951          2.8974
v  TempC                   -4.5485          322.45          220.84          218.29
v  CourantNb               0.98611          2.0508          1.0004          1.0001
v  FourierNb             0.0053422         0.11377        0.022084        0.016743
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0087162       0.0024095        0.003062


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0926          1.0225          1.0169


 TIME FOR THE TIME STEP               95:        0.17103E+02

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


 INSTANT    0.960000000E+00   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49424E-01 0.17621E+00
   Friction velocity        uk    :  0.49424E-01 0.17621E+00
   Dimensionless distance   yplus :  0.27051E+01 0.15178E+02
   Friction thermal sca.    tstar :  0.79697E+00 0.60034E+02
   Rough dim-less th. sca.  tplus :  0.20183E+01 0.11325E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35400E-01      19   0.63549E-02   0.53421E-02 0.15185E+01 
c  Velocity[X]                                      0.43617E-02 
c  Velocity[Y]                                      0.47415E-03 
c  Velocity[Z]                                      0.50625E-03 
c  Pressure     0.66711E-04     646   0.27861E-02   0.16495E+00 0.12295E+01 
c  TempC        0.86223E+04      21   0.69889E-02   0.16585E+04 0.32387E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048765                          1487


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.15773          2.0735         0.96309         0.99849
v  Velocity[Y]            -0.45062         0.48123      -0.0010521      -0.0008795
v  Velocity[Z]             -0.6273         0.17582      -0.0056626       -0.004439
v  ǁVelocityǁ            0.16197          2.1119         0.96425         0.99911
v  Pressure               0.025249          3.2265          2.9041          2.9063
v  TempC                   -10.147          322.65          220.15          217.47
v  CourantNb                     1          2.0506          1.0004          1.0001
v  FourierNb             0.0053418         0.11337        0.022097        0.016746
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0089707       0.0024104        0.003062


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0924          1.0225          1.0169


 TIME FOR THE TIME STEP               96:        0.18310E+02

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


 INSTANT    0.970000000E+00   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49013E-01 0.17614E+00
   Friction velocity        uk    :  0.49013E-01 0.17614E+00
   Dimensionless distance   yplus :  0.23801E+01 0.14955E+02
   Friction thermal sca.    tstar :  0.82047E+00 0.59968E+02
   Rough dim-less th. sca.  tplus :  0.17758E+01 0.11158E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35411E-01      19   0.63062E-02   0.52078E-02 0.14843E+01 
c  Velocity[X]                                      0.42505E-02 
c  Velocity[Y]                                      0.46612E-03 
c  Velocity[Z]                                      0.49124E-03 
c  Pressure     0.65611E-04     518   0.26147E-02   0.16237E+00 0.53877E+00 
c  TempC        0.86007E+04      21   0.71664E-02   0.16459E+04 0.32346E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048917                          1490


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              0.1488          2.0702         0.96284         0.99849
v  Velocity[Y]            -0.45196         0.48108      -0.0010574     -0.00088924
v  Velocity[Z]            -0.63384         0.17512      -0.0056764      -0.0044489
v  ǁVelocityǁ            0.15391          2.1063           0.964         0.99912
v  Pressure              0.0028837          3.2309          2.9075          2.9098
v  TempC                   -16.101          323.37          219.45          216.65
v  CourantNb                     1          2.0443          1.0004          1.0001
v  FourierNb             0.0053414         0.11389        0.022108         0.01675
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0087981       0.0024112        0.003062


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0861          1.0225          1.0169


 TIME FOR THE TIME STEP               97:        0.17536E+02

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


 INSTANT    0.980000000E+00   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.47984E-01 0.17644E+00
   Friction velocity        uk    :  0.47984E-01 0.17644E+00
   Dimensionless distance   yplus :  0.28957E+01 0.15170E+02
   Friction thermal sca.    tstar :  0.81314E+00 0.60275E+02
   Rough dim-less th. sca.  tplus :  0.21605E+01 0.11319E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35420E-01      19   0.62923E-02   0.52066E-02 0.14906E+01 
c  Velocity[X]                                      0.42224E-02 
c  Velocity[Y]                                      0.46914E-03 
c  Velocity[Z]                                      0.51509E-03 
c  Pressure     0.68241E-04     682   0.29630E-02   0.16922E+00 0.15901E+01 
c  TempC        0.85790E+04      21   0.69436E-02   0.16404E+04 0.32330E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048968                          1491


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.13413          2.0804         0.96258         0.99849
v  Velocity[Y]            -0.46512          0.4792      -0.0010655      -0.0008991
v  Velocity[Z]            -0.62666          0.1896      -0.0056882      -0.0044566
v  ǁVelocityǁ            0.14033          2.1189         0.96375         0.99912
v  Pressure               0.022205          3.2435          2.9193          2.9216
v  TempC                   -4.0475          323.22          218.76          215.83
v  CourantNb                     1          2.0421          1.0004          1.0001
v  FourierNb              0.005341         0.11415         0.02212        0.016753
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0089721       0.0024121       0.0030619


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0839          1.0225          1.0169


 TIME FOR THE TIME STEP               98:        0.20640E+02

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


 INSTANT    0.990000000E+00   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.46207E-01 0.17663E+00
   Friction velocity        uk    :  0.46207E-01 0.17663E+00
   Dimensionless distance   yplus :  0.27326E+01 0.14984E+02
   Friction thermal sca.    tstar :  0.78197E+00 0.60196E+02
   Rough dim-less th. sca.  tplus :  0.20388E+01 0.11180E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35430E-01      19   0.63683E-02   0.52005E-02 0.14924E+01 
c  Velocity[X]                                      0.42290E-02 
c  Velocity[Y]                                      0.46673E-03 
c  Velocity[Z]                                      0.50482E-03 
c  Pressure     0.65486E-04     572   0.26371E-02   0.16258E+00 0.75393E+00 
c  TempC        0.85574E+04      21   0.68415E-02   0.16134E+04 0.32165E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048684                          1494


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.13114          2.0845         0.96233          0.9985
v  Velocity[Y]            -0.46948         0.48232      -0.0010734     -0.00090973
v  Velocity[Z]              -0.628         0.17681      -0.0056975      -0.0044641
v  ǁVelocityǁ            0.13628          2.1212          0.9635         0.99913
v  Pressure               0.013958          3.2459          2.9246          2.9269
v  TempC                   -7.0142          323.56          218.07          215.01
v  CourantNb                     1          2.0541          1.0004          1.0001
v  FourierNb             0.0053405         0.11456        0.022132        0.016757
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0089292        0.002413       0.0030619


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0959          1.0226          1.0169


 TIME FOR THE TIME STEP               99:        0.17146E+02

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


 INSTANT    0.100000000E+01   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2296        -0.471448000E-01
Smooth wall               5       33794         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       22430         0.000000000E+00
Free outlet               3        2296         0.471447996E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.45853E-01 0.17684E+00
   Friction velocity        uk    :  0.45853E-01 0.17684E+00
   Dimensionless distance   yplus :  0.24914E+01 0.15181E+02
   Friction thermal sca.    tstar :  0.72729E+00 0.60417E+02
   Rough dim-less th. sca.  tplus :  0.18588E+01 0.11327E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      33794
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration        100, Physical time    0.10000E+01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
 End writing


 Time for restart files:    0.17100E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35439E-01      19   0.61231E-02   0.52837E-02 0.14991E+01 
c  Velocity[X]                                      0.43022E-02 
c  Velocity[Y]                                      0.47026E-03 
c  Velocity[Z]                                      0.51126E-03 
c  Pressure     0.66448E-04     607   0.27147E-02   0.16540E+00 0.93416E+00 
c  TempC        0.85357E+04      21   0.69880E-02   0.16054E+04 0.32170E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  TempC          
a  Local Time Step      0.00048716                          1497


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.12188          2.0826         0.96208          0.9985
v  Velocity[Y]            -0.46821         0.48114      -0.0010792      -0.0009199
v  Velocity[Z]             -0.6253         0.18841      -0.0057093      -0.0044725
v  ǁVelocityǁ            0.12792          2.1216         0.96325         0.99913
v  Pressure               0.024861          3.2525          2.9313          2.9336
v  TempC                   -8.9894          326.12          217.38          214.19
v  CourantNb                     1          2.0527          1.0004          1.0001
v  FourierNb             0.0053402         0.11459        0.022144         0.01676
v  total_pressure      1.0133e+005     1.0133e+005     1.0133e+005     1.0133e+005
v  Local Time Step           0.001       0.0092595       0.0024139       0.0030619


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0053          2.0945          1.0226          1.0169


 TIME FOR THE TIME STEP              100:        0.18356E+02

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



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



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


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




   ** TIME FOR FINAL WRITING:    0.10000E-02
      -----------------------                                



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




                      END OF CALCULATION                     
                      ==================                     


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

 Destroying structures and ending computation


Calculation time summary:

  CPU time:                1899.502 s
  Total CPU time:          5698.508 s

  Elapsed time:            1899.503 s
  CPU / elapsed time          1.000

Memory use summary:

  Theoretical instrumented dynamic memory:       416.863 MiB
                             local minimum:      138.325 MiB  (rank 2)
                             local maximum:      140.157 MiB  (rank 1)
